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  <front>
    <journal-meta>
      <journal-id journal-id-type="publisher-id">IJAR</journal-id>
      <journal-title-group>
        <journal-title>Indonesian Journal of Advanced Research</journal-title>
      </journal-title-group>
      <issn pub-type="epub">2986-0768</issn>
      <publisher>
        <publisher-name>Formosa Publisher</publisher-name>
      </publisher>
    </journal-meta>
    <article-meta>
      <article-id pub-id-type="doi">10.55927/ijar.v4i6.14678</article-id>
      <title-group>
        <article-title>Analysis of Green Oxidizer Utilization in Composite Propellants and Its Implications for the Resilience of National Defense Systems</article-title>
      </title-group>
      <contrib-group>
        <contrib contrib-type="author">
          <name>
            <surname>Ilmi</surname>
            <given-names>Nurul</given-names>
          </name>
          <aff>Program of Defense Industry, Faculty of Engineering and Technology, Republic of Defense University</aff>
          <email>nurul.ilmi@tp.idu.ac.id</email>
        </contrib>
        <contrib contrib-type="author">
          <name>
            <surname>Siahaan</surname>
            <given-names>Timbul</given-names>
          </name>
          <aff>Program of Defense Industry, Faculty of Engineering and Technology, Republic of Defense University</aff>
        </contrib>
        <contrib contrib-type="author">
          <name>
            <surname>Putra</surname>
            <given-names>I Nengah</given-names>
          </name>
          <aff>Program of Defense Industry, Faculty of Engineering and Technology, Republic of Defense University</aff>
        </contrib>
        <contrib contrib-type="author">
          <name>
            <surname>Putra</surname>
            <given-names>Rizky Dwiandra</given-names>
          </name>
          <aff>Program of Defense Industry, Faculty of Engineering and Technology, Republic of Defense University</aff>
        </contrib>
        <contrib contrib-type="author">
          <name>
            <surname>Haryanto</surname>
            <given-names>Aris</given-names>
          </name>
          <aff>Program of Defense Industry, Faculty of Engineering and Technology, Republic of Defense University</aff>
        </contrib>
      </contrib-group>
      <pub-date pub-type="epub">
        <day>20</day>
        <month>06</month>
        <year>2025</year>
      </pub-date>
      <history>
        <date date-type="received">
          <day>04</day>
          <month>05</month>
          <year>2025</year>
        </date>
        <date date-type="rev-recd">
          <day>19</day>
          <month>05</month>
          <year>2025</year>
        </date>
        <date date-type="accepted">
          <day>20</day>
          <month>06</month>
          <year>2025</year>
        </date>
      </history>
      <volume>4</volume>
      <issue>6</issue>
      <fpage>639</fpage>
      <lpage>656</lpage>
      <abstract>
        <p>The development of environmentally friendly propellant technology has become a primary focus in the defense industry. Composite propellants, which have traditionally relied on Ammonium Perchlorate (AP), offer high performance but pose environmental concerns due to the emission of corrosive chlorine compounds. This study aims to evaluate the potential use of green oxidizers such as Ammonium Dinitramide (ADN), Hydrazinium Nitroformate (HNF), hexahydro-1,3,5-trinitro-1,3,5-triazine (RDX), and octahydro-1,3,5,7-tetranitro-1,3,5,7-tetrazocine (HMX) as alternatives to AP. A qualitative literature review method was employed, drawing from various national and international scientific sources. Findings show that ADN and HNF offer promising performance and are more eco-friendly due to no chlorine emissions. However, challenges like thermal stability, hygroscopicity, and high production costs remain. This research highlights the potential of green oxidizers to reduce pollution and enhance national defense industry sustainability.</p>
      </abstract>
      <kwd-group>
        <kwd>Composite Propellant</kwd>
        <kwd>Ammonium Perchlorate</kwd>
        <kwd>Green Oxidizer</kwd>
        <kwd>Defense Industry</kwd>
      </kwd-group>
      <permissions>
        <license>
          <ali:license_ref xmlns:ali="http://www.niso.org/schemas/ali/1.0/">http://creativecommons.org/licenses/by/4.0/</ali:license_ref>
          <license-p>This is an open-access article distributed under the terms of the Creative Commons Attribution 4.0 International License.</license-p>
        </license>
      </permissions>
    </article-meta>
  </front>
  <body>
 <sec>
  <title>INTRODUCTION</title>
  <p>The strength of a nation's defense system heavily depends on the
  technology employed in its primary weapons systems (alutsista),
  including rocket and missile technology. One of the key components of
  these systems is the propellant. In general, solid composite
  propellants consist primarily of an oxidizer, which can make up to 80%
  of the total composition (Ardianingsih &amp; Kumoro, 2019). The
  remainder typically includes a fuel binder (approximately 18%),
  aluminum powder (around 10%), and additional additives such as IPDI (a
  cross-linker), comprising about 2% (Sharabi et al., 2022). Among these
  components, the oxidizer is the most dominant by volume and plays a
  critical role in supplying oxygen for combustion, particularly in
  oxygen deficient environments such as outer space.</p>
  <p><inline-graphic mimetype="image" mime-subtype="png" xlink:href="vertopal_788aa2bf547246e0b578d3f1fbc35274/media/image3.png" /><inline-graphic mimetype="image" mime-subtype="png" xlink:href="vertopal_788aa2bf547246e0b578d3f1fbc35274/media/image4.png" /><inline-graphic mimetype="image" mime-subtype="png" xlink:href="vertopal_788aa2bf547246e0b578d3f1fbc35274/media/image5.png" /><inline-graphic mimetype="image" mime-subtype="png" xlink:href="vertopal_788aa2bf547246e0b578d3f1fbc35274/media/image6.png" /><inline-graphic mimetype="image" mime-subtype="png" xlink:href="vertopal_788aa2bf547246e0b578d3f1fbc35274/media/image7.png" /><inline-graphic mimetype="image" mime-subtype="png" xlink:href="vertopal_788aa2bf547246e0b578d3f1fbc35274/media/image8.png" /><inline-graphic mimetype="image" mime-subtype="png" xlink:href="vertopal_788aa2bf547246e0b578d3f1fbc35274/media/image9.png" /><inline-graphic mimetype="image" mime-subtype="png" xlink:href="vertopal_788aa2bf547246e0b578d3f1fbc35274/media/image10.png" /></p>
  <disp-quote>
    <p><bold>Figure 1.</bold> Composition of Composite Propellants
    Source: Team Author, 2025</p>
  </disp-quote>
  <p>Ammonium Perchlorate (AP) is the most widely used oxidizer due to
  its stability and high specific impulse performance (Lysien, 2021).
  However, AP combustion produces chlorine-containing gases (such as
  HCl), which are corrosive and harmful to both human health and the
  environment (Hello Sehat, 2023). According to the U.S. Environmental
  Protection Agency (EPA, 2014), perchlorate including Ammonium
  Perchlorate is highly soluble in water, stable, and mobile in both
  surface and groundwater systems. As a result, perchlorate plumes can
  spread extensively, as seen at the Olin flare facility in Morgan Hill,
  California, where contamination extended over 9 miles. While
  perchlorate does not readily volatilize into the atmosphere from water
  or soil, it can deposit through wet or dry precipitation if released
  directly into the air (ATSDR, 2008).</p>
  <p>The use of perchlorates in industries such as the manufacture,
  testing, and disposal of ammunition and rocket fuel has led to high
  perchlorate concentrations, especially in defense-related sites both
  current and former (ATSDR, 2008). Disposal practices like dumping
  ammunition in waste pits or open burning have further contributed to
  perchlorate release into the environment (EPA, 2014).</p>
  <p>For these reasons, there is a growing need to identify safer and
  more environmentally friendly oxidizing agents commonly referred to as
  green oxidizers. Several compounds, including Ammonium Dinitramide
  (ADN), Hydrazinium Nitroformate (HNF),
  hexahydro-1,3,5-trinitro-1,3,5-triazine (RDX), and
  octahydro-1,3,5,7-tetranitro-1,3,5,7-tetrazocine (HMX), are being
  actively studied as alternative oxidizers (Abdillah et al., 2018). For
  example, ADN can achieve a specific impulse (Isp) greater than 250
  seconds and does not</p>
  <p>emit chlorine during combustion, making it a strong candidate to
  replace AP (Bohn, 2002). Nevertheless, green oxidizers also face
  challenges, including limited thermal stability, hygroscopic
  properties, and complex, costly synthesis processes. Internationally,
  NASA's Green Propellant Infusion Mission (GPIM) has successfully
  tested Hydroxylammonium Nitrate (HAN), known as AF- M315E, as a safer
  alternative to hydrazine (NASA, 2023).</p>
  <p>For Indonesia, which is striving for self-reliance in the defense
  industry, developing composite propellants based on green oxidizers
  could be a strategic move. Currently, AP is still largely imported. If
  Indonesia can develop and produce its own alternative oxidizers, this
  would not only address technical needs but also strengthen national
  strategic and economic positioning. Furthermore, national research
  policies are increasingly aligned with sustainable, locally sourced
  defense technology development.</p>
  <p>Based on this background, the objective of this study is to review
  and analyze various literature sources on the use of green oxidizers
  in composite propellants, and to evaluate their potential and
  implications for the endurance of national defense systems
  technically, environmentally, and strategically in the long term.</p>
</sec>












<sec>
  <title>LITERATURE REVIEW</title>
  <sec id="the-nasional-defense-system">
    <title>The Nasional Defense System</title>
    <p>The national defense system is a unified system designed to
    protect state sovereignty, maintain territorial integrity, and
    protect the safety of the nation from threats both from within and
    outside the country (Kemhan, 2016). This system includes military
    and non-military aspects that are synergistically integrated in
    facing various forms of strategic, tactical, and operational threats
    (Harsono et al., 2018). The success of this system relies heavily on
    the integration of technical aspectssuch as the development of
    reliable defense equipment technologies, including propellants and
    oxidizers and strategic elements that support the independence of
    the defense industry (Dirloman et al., 2020). Moreover, addressing
    environmental impacts is a crucial component in building a
    sustainable defense system, where green technology innovations
    contribute to reducing pollution risks while enhancing national
    resilience by decreasing reliance on imports (Chen et al., 2023;
    Bohn, 2002).</p>
  </sec>
  <sec id="composite-propellant-and-oxidizer">
    <title>Composite Propellant and Oxidizer</title>
    <p>Composite propellants are solid fuels composed of several main
    components such as oxidizers, fuel, and binders. The oxidizer serves
    as the oxygen provider for the combustion reaction, especially in
    oxygen-deficient environments such as outer space (Ardianingsih
    &amp; Kumoro, 2019). Ammonium Perchlorate (AP) is the most widely
    used oxidizer in composite propellants due to its stability and high
    specific impulse value (Lysien, 2021). However, AP combustion
    produces chlorine gas emissions that are corrosive and harmful to
    the environment (EPA, 2014). Therefore, the demand for
    environmentally friendly oxidizers has emerged as a major challenge
    in the future development of propellants.</p>
    <disp-quote>
      <p><italic>H1 = Green oxidizer performance affects composite
      propellant efficiency</italic></p>
    </disp-quote>
  </sec>
  <sec id="green-oxidizer-theory-and-environmental-impact">
    <title>Green Oxidizer Theory and Environmental Impact</title>
    <p>Explanation of theory here green oxidizers are oxidizing agents
    that do not produce harmful emissions such as chlorine and have the
    potential to improve combustion efficiency (Bohn, 2002). ADN and
    HNF, as examples of green oxidizers, demonstrate high specific
    impulse values as well as cleaner gas emission compositions compared
    to AP. However, these green oxidizers have drawbacks such as high
    hygroscopicity and low thermal stability, which present significant
    barriers to their use in the defense industry (Chen et al.,
    2023).</p>
    <disp-quote>
      <p><italic>H2 = Green oxidizer impact influences defense system
      sustainability.</italic></p>
    </disp-quote>
  </sec>
  <sec id="strategic-importance-for-national-defense">
    <title>Strategic Importance for National Defense</title>
    <p>The development of green oxidizers also has strategic
    implications, namely reducing dependence on imported raw materials
    such as AP, strengthening the independence of the national defense
    industry, and increasing national logistics and security resilience
    (Dirloman et al., 2020; Harsono et al., 2018). Collaboration between
    the defense industry and research institutions is key to
    accelerating the adoption of this technology.</p>
    <disp-quote>
      <p><italic>H3 = Strategic development of green
      oxidizers</italic></p>
    </disp-quote>
  </sec>
  <sec id="conceptual-framework">
    <title>Conceptual Framework</title>
    <p>This conceptual framework is designed to illustrate the
    relationship between the main variables in this study—technical,
    environmental, and strategic factors that influence the
    implementation of green oxidizers in composite propellants. The
    conceptual framework can be explained as follows based on the
    previous description:</p>
    <graphic mimetype="image" mime-subtype="jpeg" xlink:href="vertopal_788aa2bf547246e0b578d3f1fbc35274/media/image11.jpeg" />
    <disp-quote>
      <p><bold>Figure 2.</bold> Conceptual Framework</p>
    </disp-quote>
  </sec>
</sec>













<sec>
  <title>METHODOLOGY</title>
  <p>This study employs a systematic literature review approach using a
  qualitative method, guided by the PRISMA framework (Preferred
  Reporting Items for Systematic Reviews and Meta-Analyses). The
  research focuses on analyzing the use of green oxidizers in composite
  propellants and their implications for the resilience of national
  defense systems by synthesizing findings from prior research,
  scientific articles, and other relevant documents.</p>
  <p>This approach was selected because the primary aim of the study is
  knowledge mapping, conceptual analysis, and critical reflection on
  existing research, without conducting laboratory experiments (Snyder,
  2019).</p>
  <p>A systematic literature review is a structured method used to
  identify, evaluate, and synthesize previous research findings, with
  the goal of building a theoretical foundation and identifying research
  gaps for future exploration (Boell &amp; Dubravka, 2015). In this
  study, the qualitative approach is applied to explore reflectively and
  critically various technical, environmental, and strategic issues
  related to the development of green oxidizers as alternatives to
  Ammonium Perchlorate (AP). Data were collected through a systematic
  search of national and international journal databases. Keywords used
  in the search included green oxidizer, eco-friendly oxidizer,
  composite propellant, ADN, HAN, HNF, propellant sustainability, and
  defense technology. The gathered literature was then analyzed
  systematically by categorizing information based on research topics.
  The selected literature was classified into three main themes:
  performance characteristics, environmental impact, and strategic
  implications for defense industry self-reliance. The results of this
  analysis are presented in the form of analytical narrative, tables,
  and supporting figures to illustrate the core issues examined (Yang,
  2024).</p>
  <p>From the initial search, 127 articles were identified. After the
  removal of duplicates and a screening of titles and abstracts for
  relevance, 85 records remained. These were further assessed, and 53
  full-text articles were evaluated for eligibility. Ultimately, 28
  studies met the inclusion criteria and were included in the final
  synthesis.</p>
  <graphic mimetype="image" mime-subtype="jpeg" xlink:href="vertopal_788aa2bf547246e0b578d3f1fbc35274/media/image12.jpeg" />
  <disp-quote>
    <p><bold>Figure 3</bold>. PRISMA Flow Diagram – Article Selection
    Process Source: Team Author, 2025</p>
  </disp-quote>
</sec>













<sec>
  <title>RESEARCH RESULT</title>
  <p>Composite propellants continue to evolve, particularly within the
  defense industry, which prioritizes high performance while also
  addressing</p>
  <p>safety and environmental concerns. One of the key components of
  composite propellants is the oxidizer, which supplies oxygen during
  the combustion process. Ammonium Perchlorate (AP) is the most widely
  used oxidizer due to its well-known stability and its ability to
  deliver a high specific impulse, typically ranging from 262 - 266 s
  (Sutton &amp; Biblarz, 2017). However, AP combustion also generates
  chlorine-based gases such as hydrogen chloride (HCl), which are
  corrosive and pose significant environmental risks. For this research,
  more environmentally friendly alternatives or green oxidizer such as
  ADN, HNF, RDX, and HMX have been developed as potential replacements
  for AP. These compounds not only reduce chlorine emissions but also
  offer strong thermal performance and favorable specific impulse
  characteristics, although they still face challenges such as thermal
  stability issues and high production costs.</p>
  <sec id="characteristics-and-environmental-impact-of-various-green-oxidizers">
    <title>Characteristics and Environmental Impact of Various Green
    Oxidizers</title>
    <p>As one of the primary components accounting for more than 50% of
    the total mass of a propellant, oxidizers are compounds with high
    oxygen content that release a significant amount of energy
    (Abdillah, 2018). Consequently, oxidizers play a crucial role in
    determining combustion performance, storage stability, and
    environmental impact. To date, Ammonium Perchlorate (AP) has been
    the most commonly used oxidizer due to its stability and high
    specific impulse. However, as previously mentioned, AP poses
    environmental concerns, particularly related to chlorine emissions
    and groundwater contamination.</p>
    <p>In the search for more environmentally friendly alternatives to
    AP, several compounds such as Ammonium Dinitramide (ADN),
    Hydrazinium Nitroformate (HNF),
    hexahydro-1,3,5-trinitro-1,3,5-triazine (RDX), and
    octahydro-1,3,5,7-tetranitro-1,3,5,7-tetrazocine (HMX) have emerged
    as potential oxidizers. These four compounds are known for their
    high energy potential and produce significantly lower chlorine
    emissions during combustion. Table 1 presents a comparison of key
    characteristics of these oxidizers based on findings from the
    literature.</p>
<table-wrap id="tab1">
    <label>Table 1</label>
    <caption>
        <title>Comparison of Green Oxidizer Characteristics with Ammonium Perchlorate (AP)</title>
    </caption>
    <table>
        <colgroup>
            <col width="17%"/>
            <col width="15%"/>
            <col width="16%"/>
            <col width="19%"/>
            <col width="17%"/>
            <col width="17%"/>
        </colgroup>
        <thead>
            <tr>
                <th>Oxidizer</th>
                <th><bold>AP</bold></th>
                <th><bold>ADN</bold></th>
                <th><bold>HNF</bold></th>
                <th><bold>RDX</bold></th>
                <th><bold>HMX</bold></th>
            </tr>
        </thead>
        <tbody>
            <tr>
                <td>Chemical Formula</td>
                <td>NH₄ClO₄</td>
                <td>NH₄N(NO₂)₂</td>
                <td>N₂H₅C(NO₂)₃</td>
                <td>C₃H₆N₆O₆</td>
                <td>C₄H₈N₈O₈</td>
            </tr>
            <tr>
                <td>Isp (s)</td>
                <td>262 – 266</td>
                <td>255 – 265</td>
                <td>270 – 300</td>
                <td>250 – 300</td>
                <td>280 – 310</td>
            </tr>
            <tr>
                <td>ρ (g/cm³)</td>
                <td>1.74</td>
                <td>1.81</td>
                <td>1.91</td>
                <td>1.82</td>
                <td>1.96</td>
            </tr>
            <tr>
                <td>Tc (K)</td>
                <td>3371</td>
                <td>3075</td>
                <td>3080</td>
                <td>3292</td>
                <td>3271</td>
            </tr>
            <tr>
                <td>Tm (°C)</td>
                <td>230</td>
                <td>93</td>
                <td>124</td>
                <td>&gt; 170</td>
                <td>275</td>
            </tr>
            <tr>
                <td>O₂ – Balance (%)</td>
                <td>+34.04</td>
                <td>+25.8</td>
                <td>+13.1</td>
                <td>-21.61</td>
                <td>-21.63</td>
            </tr>
            <tr>
                <td>ΔHf (Kj/mol)</td>
                <td>-295.8</td>
                <td>-149.8</td>
                <td>-76.9</td>
                <td>+61.53</td>
                <td>+75.02</td>
            </tr>
            <tr>
                <td>Heat of Formation (kcal/kg)</td>
                <td>-601</td>
                <td>-282</td>
                <td>-94</td>
                <td>+72</td>
                <td>+61</td>
            </tr>
            <tr>
                <td>Mc (kg/mol)</td>
                <td>117.489</td>
                <td>124.056</td>
                <td>183.081</td>
                <td>222</td>
                <td>296</td>
            </tr>
            <tr>
                <td>Environmental Impact</td>
                <td>Produces chlorine and particulate emissions, potential for ozone depletion</td>
                <td>Less harmful than AP, produces fewer toxic byproducts</td>
                <td>Potential for reduced emissions, but still toxic</td>
                <td>High toxicity, environmental concern in military applications</td>
                <td>Similar environmental impact to RDX, toxic byproducts</td>
            </tr>
            <tr>
                <td>References</td>
                <td>Bohn (2002), Sutton and Biblarz (2017)</td>
                <td>Bohn (2002), Cican and Mitrache (2017)</td>
                <td>Bohn (2002), Louwers (1997), Zhang et al (2021)</td>
                <td>Bohn (2002), Louwers (1997), Zhang et al (2021)</td>
                <td>Bohn (2002), Louwers (1997), Zhang et al (2021)</td>
            </tr>
        </tbody>
    </table>
</table-wrap>
    <p>Source : <italic>Team Author</italic>, 2025 based on Bohn (2002);
    Cican &amp; Mitrache (2017); Louwers (1997); Sutton &amp; Biblarz
    (2017); Zhang et al. (2021).</p>
    <p>Table 1 presents a comparison of the characteristics of several
    oxidizers that may serve as environmentally friendly alternatives to
    Ammonium Perchlorate (AP) in solid propellants. The oxidizers
    reviewed include Ammonium Dinitramide (ADN), Hydrazinium
    Nitroformate (HNF), and high- energy compounds such as RDX and HMX.
    Based on thermodynamic characteristics, it can be observed that ADN
    and HNF demonstrate superior performance compared to AP,
    particularly in terms of specific impulse (Isp) and oxygen balance.
    A higher Isp indicates a greater ability to generate thrust per unit
    mass of propellant (Frem, 2018). ADN and HNF exhibit Isp values
    exceeding 265 seconds, highlighting their potential as alternative
    oxidizers. Additionally, their positive oxygen balance suggests more
    complete combustion, which contributes to improved overall
    propulsion system efficiency (Bohn, 2002).</p>
    <p>In terms of thermal stability, AP remains superior; however, ADN
    offers a more optimal balance between stability and performance.
    While HNF also achieves a high Isp, it presents storage stability
    challenges. Its melting point, approximately 124°C, makes it more
    sensitive to temperature fluctuations compared to AP (230°C) and HMX
    (275°C). This increases the risk of premature degradation or
    unintended reactions under suboptimal storage conditions.</p>
    <p>From the standpoint of combustion temperature (Tc), AP excels
    with a value of 3371 K. However, ADN and HNF record values of 3075 K
    and 3080 K, respectively still within an efficient range for solid
    propellant combustion. This demonstrates that although AP is
    thermally robust, green oxidizers such as ADN and HNF can still
    deliver competitive performance, provided they are properly
    integrated with a suitable binder system in rocket.</p>
    <p>The environmental aspect is a critical factor in evaluating
    oxidizer selection. To assess whether an oxidizer is environmentally
    friendly, it is essential to examine its combustion reaction. Table
    2 presents the general combustion reactions of each oxidizer.</p>
    <disp-quote>
      <p><bold>Table 2.</bold> Oxidizer Combustion Reactions and
      Chlorine Emission Content</p>
    </disp-quote>
    <table-wrap>
      <table>
        <colgroup>
          <col width="19%" />
          <col width="27%" />
          <col width="18%" />
          <col width="13%" />
          <col width="23%" />
        </colgroup>
        <thead>
          <tr>
            <th><p specific-use="wrapper">
              <disp-quote>
                <p><bold>Oxidizer</bold></p>
              </disp-quote>
            </p></th>
            <th><p specific-use="wrapper">
              <disp-quote>
                <p><bold>Reaction</bold></p>
              </disp-quote>
            </p></th>
            <th><p specific-use="wrapper">
              <disp-quote>
                <p><bold>Combustion Products</bold></p>
              </disp-quote>
            </p></th>
            <th><p specific-use="wrapper">
              <disp-quote>
                <p><bold>Chlorine Emission</bold></p>
              </disp-quote>
            </p></th>
            <th><p specific-use="wrapper">
              <disp-quote>
                <p><bold>Emplicative</bold></p>
              </disp-quote>
            </p></th>
          </tr>
        </thead>
        <tbody>
          <tr>
            <td><p><bold>AP</bold></p>
            <p>(NH₄ClO₄)</p></td>
            <td><p specific-use="wrapper">
              <disp-quote>
                <p>NH₄ClO₄ → N₂ + H₂O</p>
                <p>+ HCl + O₂</p>
              </disp-quote>
            </p></td>
            <td><p specific-use="wrapper">
              <disp-quote>
                <p>HCl, H₂O, N₂,</p>
                <p>O₂</p>
              </disp-quote>
            </p></td>
            <td>Present</td>
            <td><p specific-use="wrapper">
              <disp-quote>
                <p>HCl is acidic and corrosive</p>
              </disp-quote>
            </p></td>
          </tr>
          <tr>
            <td><p><bold>ADN</bold></p>
            <p>(NH₄N(NO₂)₂)</p></td>
            <td><p specific-use="wrapper">
              <disp-quote>
                <p>NH₄N(NO₂)₂ → N₂ + H₂O + O₂</p>
              </disp-quote>
            </p></td>
            <td><p specific-use="wrapper">
              <disp-quote>
                <p>N₂, H₂O, O₂</p>
              </disp-quote>
            </p></td>
            <td>None</td>
            <td><p specific-use="wrapper">
              <disp-quote>
                <p>Contains no chlorine</p>
                <p>compounds</p>
              </disp-quote>
            </p></td>
          </tr>
          <tr>
            <td><p><bold>HNF</bold></p>
            <p>(N₂H₅C(NO₂)₃)</p></td>
            <td><p specific-use="wrapper">
              <disp-quote>
                <p>N₂H₅C(NO₂)₃ → N₂ + CO₂ + H₂O + O₂</p>
              </disp-quote>
            </p></td>
            <td><p specific-use="wrapper">
              <disp-quote>
                <p>N₂, CO₂, H₂O,</p>
                <p>O₂</p>
              </disp-quote>
            </p></td>
            <td>None</td>
            <td>Clean gas products with no chlorine compounds</td>
          </tr>
          <tr>
            <td><p><bold>RDX</bold></p>
            <p>(C₃H₆N₆O₆)</p></td>
            <td><p specific-use="wrapper">
              <disp-quote>
                <p>C₃H₆N₆O₆ → N₂ + CO₂ + H₂O</p>
              </disp-quote>
            </p></td>
            <td><p specific-use="wrapper">
              <disp-quote>
                <p>N₂, CO₂, H₂O</p>
              </disp-quote>
            </p></td>
            <td>None</td>
            <td><p specific-use="wrapper">
              <disp-quote>
                <p>Does not produce chlorine</p>
              </disp-quote>
            </p></td>
          </tr>
          <tr>
            <td><p><bold>HMX</bold></p>
            <p>(C₄H₈N₈O₈)</p></td>
            <td><p specific-use="wrapper">
              <disp-quote>
                <p>C₄H₈N₈O₈ → N₂ + CO₂ + H₂O</p>
              </disp-quote>
            </p></td>
            <td><p specific-use="wrapper">
              <disp-quote>
                <p>N₂, CO₂, H₂O</p>
              </disp-quote>
            </p></td>
            <td>None</td>
            <td><p specific-use="wrapper">
              <disp-quote>
                <p>Relatively clean emissions but toxic</p>
              </disp-quote>
            </p></td>
          </tr>
        </tbody>
      </table>
    </table-wrap>
    <p>Source : Team Author, 2025</p>
    <p>Based on Table 2, it is evident that only Ammonium Perchlorate
    (AP) produces chlorine-containing compounds (HCl) during combustion,
    which pose serious risks to human health and the environment (EPA,
    2014). In contrast, the other four oxidizers ADN, HNF, RDX, and HMX
    do not contain chlorine atoms in their chemical structures, making
    them significantly safer for the environment.</p>
    <p>Overall, the preceding analysis indicates that ADN and HNF
    demonstrate strong potential as replacements for AP in solid
    propellants. The use of green oxidizers contributes not only to
    reducing environmental impact but also to enhancing the endurance of
    defense systems and optimizing propulsion performance. These
    findings align with previous studies by Bohn (2002) and Louwers
    (1997), which suggest that the development of alternative oxidizers
    can strengthen the long-term sustainability and self-reliance of a
    nation’s defense capabilities.</p>
  </sec>
  <sec id="challenges-and-solutions-in-implementing-green-oxidizers">
    <title>Challenges and Solutions in Implementing Green
    Oxidizers</title>
    <p>Growing awareness of the importance of sustainable defense
    technologies has driven efforts to replace Ammonium Perchlorate (AP)
    with more environmentally friendly oxidizers. Compounds such as
    Ammonium Dinitramide (ADN), Hydrazinium Nitroformate (HNF),
    hexahydro-1,3,5- trinitro-1,3,5-triazine (RDX), and
    octahydro-1,3,5,7-tetranitro-1,3,5,7-tetrazocine (HMX) have been
    widely explored in the literature as primary alternatives, due to
    their high specific impulse and cleaner combustion products.</p>
    <p>However, transitioning from laboratory-scale research to
    full-scale industrial production presents significant challenges.
    Key obstacles include thermal stability, high production costs,
    complex synthesis processes, and the need for supporting
    infrastructure. These factors currently hinder the widespread
    implementation of green oxidizers in the defense industry.</p>
    <disp-quote>
      <p><italic>Thermal Stability and Sensitivity</italic></p>
    </disp-quote>
    <p>Green oxidizers such as Ammonium Dinitramide (ADN) and
    Hydrazinium Nitroformate (HNF) are next-generation oxidizing
    compounds currently being developed as more environmentally friendly
    alternatives to Ammonium Perchlorate (AP). ADN and HNF produce
    cleaner combustion products as they do not release corrosive and
    toxic chlorine-containing compounds. This advantage makes them
    highly promising for application in rocket propulsion systems,
    particularly in efforts to reduce the environmental footprint of the
    defense industry.</p>
    <p>Despite these benefits, both compounds have critical drawbacks,
    notably their strong hygroscopic nature and sensitivity to
    temperature and humidity. ADN, in particular, readily absorbs
    moisture from the air. This absorption process occurs in three
    stages: starting with the interaction between water vapor and the
    surface of solid ADN, followed by the formation of a thin water
    layer, and ultimately leading to deliquescence a phase in which the
    absorbed moisture forms a liquid interface with the ADN, resulting
    in its partial dissolution (Chen et al., 2023).</p>
    <graphic mimetype="image" mime-subtype="jpeg" xlink:href="vertopal_788aa2bf547246e0b578d3f1fbc35274/media/image13.jpeg" />
    <disp-quote>
      <p><bold>Figure 4.</bold> Isothermal Hygroscopic Curves of ADN at
      Different Temperatures</p>
    </disp-quote>
    <p>Source: Chen, et al., 2023</p>
    <p>The isothermal hygroscopic curves of ADN shown in Figure 3
    indicate that its moisture absorption behavior is highly dependent
    on relative humidity, temperature, and sample purity. A study by Nie
    et al. (2021), as cited in Chen et al. (2023), found that ADN begins
    to deliquesce when stored at relative humidity levels above 50% for
    less than 10 hours. The critical relative humidity for ADN was
    reported at 59%, which closely aligns with findings by Chen et al.
    (2024), who identified a critical threshold of 55.2%.</p>
    <p>In contrast, RDX and HMX are known to be non-hygroscopic but are
    highly sensitive to mechanical stimuli such as pressure and
    friction, posing significant risks if used without appropriate
    treatments such as coating or desensitization through binders.
    Furthermore, the thermal stability of RDX and HMX is limited above
    204.3°C, which must be carefully considered in the thermal design of
    rocket systems (Yang, 2024).</p>
    <p>Several approaches have been developed to reduce the
    hygroscopicity and improve the stability of ADN and HNF. One
    promising method is co- crystallization, such as forming a
    co-crystal between ADN and 3,4- diaminofurazan (DAF), which has been
    shown to reduce the hygroscopicity of ADN from 15.35% to 7.90% by
    forming hydrogen bonds that inhibit moisture uptake (Hu et al.,
    2023). For RDX and HMX, common approaches include
    microencapsulation, the use of plasticizers and elastomeric binders,
    and crystal structure modification to reduce sensitivity (Urbanski,
    1985).</p>
    <disp-quote>
      <p><italic>Complexity of Synthesis and Production
      Costs</italic></p>
    </disp-quote>
    <p>According to Bohn (2002), maintaining the stability of
    solid-state Ammonium Dinitramide (ADN) requires the use of additives
    such as polymeric solvents or complexing agents. These not only
    increase the number of processing steps but also contribute
    significantly to the total production cost. Refining the
    crystallization process of ADN to meet industrial-grade standards
    involves the re-engineering of production facilities and handling
    systems for reactive materials (Chen et al., 2024).</p>
    <p>The synthesis of Hydrazinium Nitroformate (HNF) involves
    precursors such as nitroform and hydrazinium salts, both of which
    are highly sensitive to temperature and pose explosion risks.
    Continuous cooling and highly precise pH control are essential to
    maintain reaction stability (Bohn, 2002).</p>
    <p>While RDX and HMX have been industrially produced for several
    decades, their synthesis presents its own challenges. These
    compounds are typically manufactured through heterogeneous nitration
    of heterocyclic compounds. The reagents used nitric acid and acetic
    anhydride are both highly corrosive and toxic, necessitating the use
    of chemically resistant production equipment, intensive cooling
    systems, and stringent safety protocols. Moreover, to achieve high
    purity and specific particle size requirements, multiple
    recrystallization and milling steps are needed, which further
    increase production time and cost (Agrawal, 2010).</p>
    <p>Additionally, the manufacturing processes for RDX and HMX
    generate hazardous chemical waste, including acidic wastewater and
    reactive solids. This significantly increases the cost burden due to
    the need for chemical waste treatment systems and compliance with
    environmental regulations.</p>
    <disp-quote>
      <p><italic>Regulation and Certification</italic></p>
    </disp-quote>
    <p>Regulatory challenges often hinder the adoption of
    environmentally friendly processes. Current regulations tend to
    focus on risk reduction through exposure control, while green
    chemistry emphasizes the reduction of inherent risk by minimizing
    hazard. In the United States, regulations require manufacturers to
    undergo recertification with the Food and Drug Administration (FDA)
    whenever production processes are altered (Ratti, 2020).</p>
    <p>This recertification process is costly and time-consuming,
    effectively discouraging companies from investing in the development
    of energy-efficient and waste-reducing chemical technologies.
    Regulatory systems that are oriented toward control rather than
    innovation impose significant financial</p>
    <p>burdens and act as barriers to process improvement. Moreover, a
    lack of awareness among various stakeholder groups further impedes
    the implementation of green processes. Successfully developing green
    chemical technologies requires not only expertise in green
    chemistry, but also in green engineering, biotechnology, economics,
    and, critically, toxicology.</p>
    <p>In Indonesia, the development of high-energy chemicals is
    regulated by government agencies such as the Ministry of Defense, as
    outlined in Ministerial Regulation No. 5 of 2016 on the Development
    and Supervision of the Explosives Industry. However, this regulation
    does not specifically address environmentally friendly propellants.
    Permitting procedures related to the production, storage, and
    transportation of high-energy chemicals still refer to conventional
    explosives and have yet to holistically incorporate the unique
    characteristics of green chemicals.</p>
    <p>To overcome regulatory barriers surrounding green chemical
    technologies, a systematic approach is needed one that fosters
    synergy among policymakers, industry, research institutions, and
    certification authorities. The Indonesian government could support
    this effort by developing national standards specifically for
    environmentally friendly high-energy chemicals, streamlining
    certification procedures for research and pilot-testing phases, and
    establishing a fast-track mechanism for green technology
    innovations.</p>
  </sec>
  <sec id="the-link-between-green-propellant-innovation-and-independent-defense-strategy">
    <title>The Link Between Green Propellant Innovation and Independent
    Defense Strategy</title>
    <p>The use of Ammonium Perchlorate (AP)-based oxidizers remains
    heavily reliant on imported supply chains. Innovations in
    alternative materials such as Ammonium Dinitramide (ADN),
    Hydroxylammonium Nitrate (HAN), RDX, and HMX create opportunities to
    reduce this dependence and promote national self-reliance in raw
    material production. The development of eco-friendly oxidizers like
    ADN contributes not only to lowering reliance on foreign suppliers
    but also to strengthening domestic defense capabilities (Dirloman et
    al., 2020).</p>
    <graphic mimetype="image" mime-subtype="jpeg" xlink:href="vertopal_788aa2bf547246e0b578d3f1fbc35274/media/image14.jpeg" />
    <p><bold>Figure 5.</bold> Diagram of the Link Between Green Oxidizer
    Innovation and National Defense Strategy</p>
    <p>Source: Team Author, 2025</p>
    <p>As illustrated in Figure 4, the availability of domestically
    produced oxidizers demonstrates that green oxidizer innovation can
    directly support national defense strategy. This innovation promotes
    raw material self- sufficiency and reduces dependence on imports.
    Moreover, the defense logistics system becomes more resilient to
    external disruptions, geopolitical conflicts, and supply chain
    interruptions. Dependence on foreign technology in the defense
    sector creates strategic vulnerabilities that can only be addressed
    through the development of national capacity based on technological
    innovation (Harsono et al., 2018).</p>
    <p>Collaboration between the defense industry and research
    institutions such as PT Dahana, PT Pindad, and the National Research
    and Innovation Agency (BRIN) holds significant potential for
    advancing green propellant technology. However, these efforts still
    require strong policy support and sustained investment to enable the
    downstream integration of such technologies into national weapon
    systems. Ultimately, this approach will strengthen the self-reliance
    of the national defense industry.</p>
  </sec>
  <sec id="strategy-for-implementing-green-oxidizers-in-indonesia">
    <title>Strategy for Implementing Green Oxidizers in
    Indonesia</title>
    <p>The development of green oxidizers as part of composite
    propellant technology must be examined not only from the perspective
    of technical performance and environmental impact, but also in terms
    of how their application can be aligned with the current state of
    Indonesia’s defense industry. Accordingly, the following discussion
    presents a case study of implementation, national data on raw
    material dependency of this technology.</p>
    <disp-quote>
      <p><italic>National Case Study: The Potential Implementation of
      Green Oxidizers by PT Dahana and PT Pindad</italic></p>
    </disp-quote>
    <p>PT Dahana, a state-owned enterprise (BUMN) specializing in
    explosives, has taken a leading role in the development of solid
    propellant technology for military applications. In its 2022 Annual
    Report, PT Dahana affirmed its commitment to supporting research on
    more environmentally friendly rocket fuels through collaborations
    with various national institutions, including BRIN and LAPAN (PT
    Dahana, 2022). Although domestic production still relies heavily on
    Ammonium Perchlorate (AP), internal experimental studies have begun
    to explore the substitution potential of Ammonium Dinitramide (ADN),
    a green oxidizer that does not emit chlorine-based compounds during
    combustion.</p>
    <p>In addition, PT Dahana has also begun developing variants of
    smokeless composite-based propellants for ammunition and tactical
    rocket applications, aimed at reducing visual signatures during
    launch and enhancing stealth characteristics in combat. These
    smokeless composite propellants are designed to minimize the
    formation of white smoke resulting from the combustion of aluminum
    or carbon-based materials and can be combined with green oxidizers
    to produce a cleaner and more efficient propulsion system (PT
    Dahana, 2023). The smokeless composite propellants are engineered to
    reduce the white smoke generated by the combustion of aluminum or
    carbon materials and can be</p>
    <p>formulated with green oxidizers such as ADN (Ammonium
    Dinitramide) or HAN (Hydroxylammonium Nitrate) to produce a cleaner
    propulsion system. The implementation of green oxidizers offers
    several advantages, such as:</p>
    <list list-type="bullet">
      <list-item>
        <p>Reducing environmental footprint and residual toxicity,
        particularly during testing and combat operations in civilian
        areas or sensitive ecosystems.</p>
      </list-item>
      <list-item>
        <p>Improving the thermodynamic performance of the propellant, as
        ADN is known to have a better oxygen balance compared to AP
        (Ammonium Perchlorate).</p>
      </list-item>
      <list-item>
        <p>Decreasing dependence on imported raw materials.</p>
      </list-item>
    </list>
    <p>In addition to PT Dahana, PT Pindad is also actively
    strengthening its expertise in energetic materials technology. In
    2023, PT Pindad established a partnership with the Bandung Institute
    of Technology (ITB) to conduct research and development on
    propellants and explosive detection devices (PT Pindad Persero,
    2022). The focus of this collaboration includes improving the
    performance and efficiency of rocket fuels as well as enhancing
    safety in the handling of explosive materials. Such collaboration
    reflects a crucial synergy between industry and academia, which
    plays a key role in accelerating national technological
    readiness.</p>
    <p>Furthermore, the collaboration between the defense industry and
    research institutions reflects a new direction in the transformation
    of national explosive materials technology. In addition to reducing
    dependence on imports, this initiative also aims to establish a
    sustainable domestic production base. The implementation of green
    oxidizer technology, such as ADN, in the national propellant systems
    is not only intended for rocket applications but can also be
    expanded to include weapon systems and small-caliber ammunition.
    Such initiatives also open opportunities for technology transfer
    from basic research to ready-to-use products that can support the
    operational readiness of the Indonesian Armed Forces (TNI).</p>
    <p>An example of early implementation could be directed toward the
    LAPAN RX-450 or RS-122B rocket systems as test platforms for
    integrating ADN as an alternative oxidizer to AP. Additionally, the
    initial phase can be carried out through a staged technology
    readiness level (TRL) scheme coordinated by the Ministry of Defense
    and the Defense Industry Policy Committee (KKIP), ensuring that the
    development of green oxidizers progresses beyond the laboratory
    stage toward industrialization and operational deployment.</p>
    <disp-quote>
      <p><italic>Dependence on Imported Propellant Raw
      Materials</italic></p>
    </disp-quote>
    <p>The performance of propellants produced by LAPAN has not yet
    reached optimal standards, which is believed to be influenced by the
    relatively low quality of domestically produced Ammonium Perchlorate
    (AP). One strategy to improve the characteristics of local AP is to
    conduct comparative analyses with imported materials, particularly
    those sourced from China and South Korea. This approach aims to
    bridge the quality gap in oxidizers and</p>
    <p>enhance the thrust performance of Indonesian-made propellants to
    meet international standards (Hutauruk, et al, 2020).</p>
    <p>Meanwhile, Indonesia remains highly dependent on imported
    propellant raw materials, especially AP from China and Russia. The
    demand for composite propellants is expected to continue increasing
    in line with the development of rockets and missiles. This is
    further supported by official data from Statistics Indonesia (Badan
    Pusat Statistik/BPS), which shows a consistent trend in the import
    of propellant raw materials specifically those classified under HS
    code 36010000 (Propellant Powders) over the past four year.</p>
    <disp-quote>
      <p><bold>Table 3.</bold> Import of Propellant Raw Materials 2021 -
      2024</p>
    </disp-quote>
    <table-wrap>
      <table>
        <colgroup>
          <col width="51%" />
          <col width="49%" />
        </colgroup>
        <thead>
          <tr>
            <th><bold>Year</bold></th>
            <th><bold>Import Quantity (kg)</bold></th>
          </tr>
        </thead>
        <tbody>
          <tr>
            <td>2021</td>
            <td>5.276.034</td>
          </tr>
          <tr>
            <td>2022</td>
            <td>3.558.587</td>
          </tr>
          <tr>
            <td>2023</td>
            <td>2.797.579</td>
          </tr>
          <tr>
            <td>2024</td>
            <td>3.244.215</td>
          </tr>
        </tbody>
      </table>
    </table-wrap>
    <disp-quote>
      <p>Source: (Badan Pusat Statistik (BPS), 2025)</p>
    </disp-quote>
    <p>The data indicates a consistent and significant reliance on
    imports. The highest import volume occurred in 2021, reaching over
    5.2 million kilograms. Although there was a decline in subsequent
    years, the import volume remained high, averaging more than 3
    million kilograms per year. These fluctuations may be influenced by
    variables such as changes in defense budget allocations, the
    dynamics of national defense equipment (alutsista) projects, or
    external factors like global prices and supply availability.</p>
    <p>This situation highlights that domestic production is still
    unable to meet propellant demands independently, both in terms of
    quality and quantity. Dependence on imported materials creates
    strategic vulnerabilities, including risks of supply chain
    disruptions due to embargoes, geopolitical conflicts, or
    international logistical barriers. To better understand the scale of
    Indonesia’s propellant needs, the annual demand composition by
    propellant type is illustrated in Figure 6 below.</p>
    <graphic mimetype="image" mime-subtype="jpeg" xlink:href="vertopal_788aa2bf547246e0b578d3f1fbc35274/media/image15.jpeg" />
    <disp-quote>
      <p><bold>Figure 6.</bold> Annual Propellant Requirement
      (tons/year)</p>
      <p>Source: Directorate General of Defense Potential, Ministry of
      Defense (2018), cited in Hutauruk et al., 2020</p>
    </disp-quote>
    <p>Figure 6 shows that national propellant demand is dominated by
    the Double Base MKK type, accounting for 55%, followed by Composite
    Rocket at 24%, and Single Base MKB at 17%. Meanwhile, Double Base
    Rocket and Double Base MKB contribute 3% and 1%, respectively. The
    Composite Rocket propellant, which makes up 24% of total demand, is
    the most common type utilizing AP (Ammonium Perchlorate) as its
    primary oxidizer.</p>
    <p>This composition indicates that the majority of Indonesia’s
    weapon systems rely heavily on AP or similar oxidizers. Therefore,
    as a long-term solution, the development of green oxidizers such as
    Ammonium Dinitramide (ADN) and Hydrazinium Nitroformate (HNF) is
    essential. These oxidizers are not only more environmentally
    friendly producing no chlorine emissions but also offer
    opportunities for domestic production through collaboration between
    industry and research institutions. This initiative would strengthen
    national defense logistics resilience, increase the local content
    (TKDN), and support sustainable development goals within the defense
    industry.</p>
  </sec>
</sec>









<sec>
 <title>DISCUSSION</title>
  <p>This study shows that green oxidizers such as Ammonium Dinitramide
  (ADN) and Hydrazinium Nitroformate (HNF) have the potential to replace
  Ammonium Perchlorate (AP), which has long been used in composite
  propellants. ADN and HNF exhibit good combustion performance with high
  specific impulse and do not produce harmful chlorine emissions, making
  them more environmentally friendly. However, the main challenges in
  using green oxidizers are their high hygroscopicity and lower thermal
  stability compared to AP, especially under storage conditions.
  Additionally, the production process of green oxidizers remains
  complex and costly, requiring innovations in manufacturing technology
  to enable efficient production. From a strategic perspective, adopting
  green oxidizers can enhance national defense industry independence by
  reducing reliance on imported raw materials. Collaboration among
  research institutions, industry, and the government is essential to
  accelerate the development and implementation of this technology.
  Therefore, the development of green oxidizers is a crucial step toward
  a more efficient and environmentally friendly defense system</p>
  <p>These overall findings affirm that the development of green
  oxidizers is a strategic step that integrates technical,
  environmental, and policy aspects. Although significant challenges
  remain, the long-term potential benefits—such as improving propellant
  efficiency, ensuring environmental sustainability, and strengthening
  national self-reliance are highly promising. Therefore, further
  research should focus on formulating more stable and cost-effective
  green oxidizers, as well as conducting field performance testing.</p>
</sec>










<sec>
  <title>CONCLUSIONS AND RECOMMENDATIONS</title>
  <p>Based on the literature review conducted, it can be concluded that
  the use of green oxidizers such as Ammonium Dinitramide (ADN) and
  Hydrazinium Nitroformate (HNF) in composite propellants presents
  significant</p>
  <p>potential as a substitute for Ammonium Perchlorate (AP), which is
  commonly used but has known negative environmental impacts. ADN and
  HNF offer high combustion performance, do not produce toxic gases such
  as chlorine, and possess an oxygen balance conducive to combustion
  efficiency.</p>
  <p>Nevertheless, several technical challenges must be taken seriously.
  ADN is highly hygroscopic, with a critical humidity point at 55.2%,
  making it unstable in tropical environments like Indonesia without
  proper storage systems. On the other hand, although RDX and HMX do not
  absorb moisture, they are highly sensitive to pressure and
  temperature, posing handling risks if not managed with strict safety
  protocols.</p>
  <p>National case studies show that Indonesia remains heavily dependent
  on imported propellant raw materials. Data from Statistics Indonesia
  (BPS) indicates that from 2021 to 2024, the volume of imported
  propellant materials (HS 36010000) consistently remained high,
  exceeding 3 million kilograms annually. This dependency poses
  potential vulnerabilities within the defense system, particularly in
  the event of embargoes or global supply disruptions.</p>
  <p>The development and utilization of green oxidizers in Indonesia is
  not only a technical and environmental necessity but also a strategic
  priority to strengthen national defense self-reliance. For this
  initiative to succeed, it requires concrete policy support in the form
  of sustained research funding, strengthened regulations and safety
  protocols for high-energy materials, and integration between research
  institutions and national strategic industries. In this way, the
  adoption of green oxidizers can become a tangible step toward a more
  independent, secure, and sustainable defense system.</p>
</sec>










<sec>
  <title>ADVANCED RESEARCH</title>
  <p>This study has limitations as it only employs a literature review
  method without conducting direct laboratory experiments or tests, thus
  the analysis results regarding the performance and stability of green
  oxidizers remain conceptual. Moreover, aspects of industrial scale
  production and long-term environmental impacts have not been
  thoroughly analyzed. Therefore, further research is recommended to
  carry out experimental studies on the formulation of green oxidizers
  that are resistant to moisture and thermally stable, as well as
  performance testing of propellants under real conditions.</p>
</sec>









<sec>
  <title>ACKNOWLEDGMENT</title>
  <p>The authors would like to express their deepest gratitude to the
  Indonesian Defense University, particularly the Defense Industry Study
  Program, for providing the scholarship support for the master’s
  program. This invaluable assistance has greatly facilitated the
  completion of this research and contributed significantly to the
  authors academic and professional development.</p>
</sec>












<sec>
      <title>REFERENCES</title>
      <ref-list>
<ref id="ref1">
  <element-citation publication-type="web">
    <person-group person-group-type="author">
      <name><surname>Agency for Toxic Substance and Disease Registry</surname><given-names></given-names></name>
    </person-group>
    <article-title>Agency for Toxic Substance and Disease Registry (ATSDR)</article-title>
    <source>www.atsdr.cdc.gov</source>
    <year>2008</year>
    <comment>[Web]</comment>
  </element-citation>
</ref>

<ref id="ref2">
  <element-citation publication-type="journal">
    <person-group person-group-type="author">
      <name><surname>Abdillah</surname><given-names>L. H.</given-names></name>
      <name><surname>Wibowo</surname><given-names>H. B.</given-names></name>
      <name><surname>Hartaya</surname><given-names>K.</given-names></name>
    </person-group>
    <article-title>Penggunaan Binder HTPB Berenergi Tinggi untuk Meningkatkan Energetik Propelan Komposit</article-title>
    <source>Journal of Teknologi Dirgantara</source>
    <year>2018</year>
    <volume>16</volume>
    <issue>1</issue>
    <fpage>35</fpage>
    <lpage>44</lpage>
    <comment>[Journal]</comment>
  </element-citation>
</ref>

<ref id="ref3">
  <element-citation publication-type="book">
    <person-group person-group-type="author">
      <name><surname>Agrawal</surname><given-names>J. P.</given-names></name>
    </person-group>
    <source>High Energy Materials: Propellants, Explosive and Pyrotechnics</source>
    <publisher-loc>Weinheim</publisher-loc>
    <publisher-name>Wiley VCH Verlag GmbH &amp; Co KGaA</publisher-name>
    <year>2010</year>
    <comment>[Book]</comment>
  </element-citation>
</ref>

<ref id="ref4">
  <element-citation publication-type="journal">
    <person-group person-group-type="author">
      <name><surname>Ardianingsih</surname><given-names>R.</given-names></name>
      <name><surname>Kumoro</surname><given-names>A. C.</given-names></name>
    </person-group>
    <article-title>Analisis Viskositas Slurry Propelan Untuk Akurasi Karakterisasi Rheologi Berbasis Perekat Hydroxy Terminated Polybutadiene Dengan Plasticizer Dioctyl Adipate</article-title>
    <source>Journal of Teknik</source>
    <year>2019</year>
    <volume>4</volume>
    <issue>3</issue>
    <fpage>154</fpage>
    <lpage>160</lpage>
    <comment>[Journal]</comment>
  </element-citation>
</ref>

<ref id="ref5">
  <element-citation publication-type="web">
    <person-group person-group-type="author">
      <name><surname>Badan Pusat Statistik</surname><given-names></given-names></name>
    </person-group>
    <article-title>Data Ekspor Impor Nasional</article-title>
    <source>https://www.bps.go.id/id/exim</source>
    <year>2025</year>
    <comment>[Web]</comment>
  </element-citation>
</ref>

<ref id="ref6">
  <element-citation publication-type="journal">
    <person-group person-group-type="author">
      <name><surname>Boell</surname><given-names>S. K.</given-names></name>
      <name><surname>Cecez-Kecmanovic</surname><given-names>D.</given-names></name>
    </person-group>
    <article-title>On Being Systematic in Literature Reviews in IS</article-title>
    <source>Journal of Information Technology</source>
    <year>2015</year>
    <volume>30</volume>
    <fpage>161</fpage>
    <lpage>173</lpage>
    <comment>[Journal]</comment>
  </element-citation>
</ref>

<ref id="ref7">
  <element-citation publication-type="journal">
    <person-group person-group-type="author">
      <name><surname>Bohn</surname><given-names>M.</given-names></name>
    </person-group>
    <article-title>Stabilization of the New Oxidizer Ammonium Dinitramide (ADN) in Solid Phase</article-title>
    <source>Chemiche Technologies</source>
    <year>2002</year>
    <comment>[Journal]</comment>
  </element-citation>
</ref>

<ref id="ref8">
  <element-citation publication-type="journal">
    <person-group person-group-type="author">
      <name><surname>Chen</surname><given-names>F.</given-names></name>
      <name><surname>Liu</surname><given-names>D.</given-names></name>
      <name><surname>Xuan</surname><given-names>C.</given-names></name>
      <!-- Others omitted for brevity -->
    </person-group>
    <article-title>Theoretical Simulation Research on The Hygroscopicity, Stability, Sensitivity, and Mechanical Properties of The Cocrystals of Ammonium Nitrate with Typical High Energetic Molecules</article-title>
    <source>Journal of Material Stoday</source>
    <year>2024</year>
    <volume>38</volume>
    <fpage>1</fpage>
    <lpage>20</lpage>
    <comment>[Journal]</comment>
  </element-citation>
</ref>

<ref id="ref9">
  <element-citation publication-type="journal">
    <person-group person-group-type="author">
      <name><surname>Chen</surname><given-names>F.</given-names></name>
      <name><surname>Xuan</surname><given-names>C.</given-names></name>
      <!-- Others omitted -->
    </person-group>
    <article-title>A Review on The High Energy Oxidizer Ammonium Dinitramide: Its Synthesis, Thermal Decomposition, Hygroscopicity, and Application in Energetic Materials</article-title>
    <source>Journal of Defense Technology</source>
    <year>2023</year>
    <volume>19</volume>
    <fpage>163</fpage>
    <lpage>195</lpage>
    <comment>[Journal]</comment>
  </element-citation>
</ref>

<ref id="ref10">
  <element-citation publication-type="journal">
    <person-group person-group-type="author">
      <name><surname>Cican</surname><given-names>G.</given-names></name>
      <name><surname>Mitrache</surname><given-names>A. D.</given-names></name>
    </person-group>
    <article-title>Rocket Solid Propellant Alternative Based on Ammonium Dinitramide</article-title>
    <source>Journal of Incas Bulletin</source>
    <year>2017</year>
    <volume>9</volume>
    <issue>1</issue>
    <fpage>17</fpage>
    <lpage>24</lpage>
    <comment>[Journal]</comment>
  </element-citation>
</ref>

<ref id="ref11">
  <element-citation publication-type="journal">
    <person-group person-group-type="author">
      <name><surname>Frem</surname><given-names>D.</given-names></name>
    </person-group>
    <article-title>A Reliable Method for Predicting the Specific Impulse of Chemical Propellants</article-title>
    <source>Journal of Technology and Management</source>
    <year>2018</year>
    <volume>10</volume>
    <fpage>1</fpage>
    <lpage>21</lpage>
    <comment>[Journal]</comment>
  </element-citation>
</ref>

<ref id="ref12">
  <element-citation publication-type="journal">
    <person-group person-group-type="author">
      <name><surname>Hu</surname><given-names>D.</given-names></name>
      <name><surname>Wang</surname><given-names>Y.</given-names></name>
      <name><surname>Xiao</surname><given-names>C.</given-names></name>
      <!-- Others omitted -->
    </person-group>
    <article-title>Studies on Ammonium Dinitramide and 3,4 Diaminofurazan Cocrystal for Tuning the Hygroscopicity</article-title>
    <source>Journal of Chinese Chemical Engineering</source>
    <year>2023</year>
    <volume>61</volume>
    <fpage>157</fpage>
    <lpage>164</lpage>
    <comment>[Journal]</comment>
  </element-citation>
</ref>

<ref id="ref13">
  <element-citation publication-type="journal">
    <person-group person-group-type="author">
      <name><surname>Hutauruk</surname><given-names>J.</given-names></name>
      <name><surname>Bura</surname><given-names>R. O.</given-names></name>
      <name><surname>Wibowo</surname><given-names>H. B.</given-names></name>
    </person-group>
    <article-title>Analisis Karakteristik Material Padat (Ammonium Perchlorat) Propelan Komposit Terhadap Kinerja Propelan Lapan</article-title>
    <source>Jurnal Teknologi Persenjataan</source>
    <year>2020</year>
    <volume>2</volume>
    <issue>1</issue>
    <fpage>51</fpage>
    <lpage>64</lpage>
    <comment>[Journal]</comment>
  </element-citation>
</ref>

<ref id="ref14">
  <element-citation publication-type="report">
    <person-group person-group-type="author">
      <name><surname>Kementerian Pertahanan Republik Indonesia</surname><given-names></given-names></name>
    </person-group>
    <article-title>Peraturan Menteri Pertahanan Nomor 5 Tahun 2016 tentang Pembinaan dan Pengembangan Industri Bahan Peledak</article-title>
    <year>2016</year>
    <comment>[Report]</comment>
  </element-citation>
</ref>

<ref id="ref15">
  <element-citation publication-type="journal">
    <person-group person-group-type="author">
      <name><surname>Louwers</surname><given-names>J.</given-names></name>
    </person-group>
    <article-title>Hydrazinium Nitroformate: A High Performance Next Generation Oxidizer</article-title>
    <source>Journal of Pyrotechnics</source>
    <year>1997</year>
    <volume>6</volume>
    <fpage>36</fpage>
    <lpage>42</lpage>
    <comment>[Journal]</comment>
  </element-citation>
</ref>

<ref id="ref16">
  <element-citation publication-type="journal">
    <person-group person-group-type="author">
      <name><surname>Lysien</surname><given-names>K.</given-names></name>
      <name><surname>Stolarczyk</surname><given-names>A.</given-names></name>
      <name><surname>Jarosz</surname><given-names>T.</given-names></name>
    </person-group>
    <article-title>Solid Propellant Formulations: A Review of Recent Progress and Utilized Components</article-title>
    <source>Journal of Materials</source>
    <year>2021</year>
    <volume>14</volume>
    <fpage>1</fpage>
    <lpage>17</lpage>
    <comment>[Journal]</comment>
  </element-citation>
</ref>

<ref id="ref17">
  <element-citation publication-type="web">
    <person-group person-group-type="author">
      <name><surname>NASA</surname><given-names></given-names></name>
    </person-group>
    <article-title>Green Propellant Infusion Mission - Project Fact Sheet</article-title>
    <source>https://www.nasa.gov</source>
    <year>2023</year>
    <comment>[Web]</comment>
  </element-citation>
</ref>

<ref id="ref18">
  <element-citation publication-type="report">
    <person-group person-group-type="author">
      <name><surname>PT Dahana Persero</surname><given-names></given-names></name>
    </person-group>
    <article-title>Laporan Tahunan 2023 - Building Resilience Through Innovation</article-title>
    <publisher-name>PT Dahana</publisher-name>
    <publisher-loc>Subang</publisher-loc>
    <year>2023</year>
    <comment>[Report]</comment>
  </element-citation>
</ref>

<ref id="ref19">
  <element-citation publication-type="report">
    <person-group person-group-type="author">
      <name><surname>PT Dahana Persero</surname><given-names></given-names></name>
    </person-group>
    <article-title>Laporan Tahunan 2022</article-title>
    <publisher-name>PT Dahana</publisher-name>
    <publisher-loc>Subang, Jawa Barat</publisher-loc>
    <year>2022</year>
    <comment>[Report]</comment>
  </element-citation>
</ref>

<ref id="ref20">
  <element-citation publication-type="web">
    <person-group person-group-type="author">
      <name><surname>PT Pindad Persero</surname><given-names></given-names></name>
    </person-group>
    <article-title>PT Pindad Jalin Kerjasama dengan ITB Kembangkan Riset Propelan dan Alat Pendeteksi Bahan Peledak</article-title>
    <source>https://pindad.com</source>
    <year>2022</year>
    <comment>[Web]</comment>
  </element-citation>
</ref>

<ref id="ref21">
  <element-citation publication-type="journal">
    <person-group person-group-type="author">
      <name><surname>Ratti</surname><given-names>R.</given-names></name>
    </person-group>
    <article-title>Industrial Applications of Green Chemistry: Status, Challenges and Prospects</article-title>
    <source>Journal of A Springer Nature</source>
    <year>2020</year>
    <volume>2</volume>
    <issue>263</issue>
    <fpage>1</fpage>
    <lpage>7</lpage>
    <comment>[Journal]</comment>
  </element-citation>
</ref>

<ref id="ref22">
  <element-citation publication-type="web">
    <person-group person-group-type="author">
      <name><surname>Sehat</surname><given-names>H.</given-names></name>
    </person-group>
    <article-title>Hello Sehat</article-title>
    <source>https://hellosehat.com</source>
    <year>2023</year>
    <comment>[Web]</comment>
  </element-citation>
</ref>

<ref id="ref23">
  <element-citation publication-type="conference">
    <person-group person-group-type="author">
      <name><surname>Sharabi</surname><given-names>N.</given-names></name>
      <name><surname>Abdalla</surname><given-names>Y.</given-names></name>
      <name><surname>Yavor</surname><given-names>Y.</given-names></name>
    </person-group>
    <article-title>Effect of Coated Nano Aluminium Powders on the Agglomeration in Solid Propellant</article-title>
    <source>European Conference for Aeronautics and Space Science (EUCASS)</source>
    <year>2022</year>
    <fpage>1</fpage>
    <lpage>20</lpage>
    <comment>[Conference]</comment>
  </element-citation>
</ref>

<ref id="ref24">
  <element-citation publication-type="journal">
    <person-group person-group-type="author">
      <name><surname>Snyder</surname><given-names>H.</given-names></name>
    </person-group>
    <article-title>Literature review as a research methodology: An overview and guidelines</article-title>
    <source>Journal of Business Research</source>
    <year>2019</year>
    <volume>104</volume>
    <fpage>333</fpage>
    <lpage>339</lpage>
    <comment>[Journal]</comment>
  </element-citation>
</ref>

<ref id="ref25">
  <element-citation publication-type="book">
    <person-group person-group-type="author">
      <name><surname>Sutton</surname><given-names>G. P.</given-names></name>
      <name><surname>Biblarz</surname><given-names></given-names></name>
    </person-group>
    <source>Rocket Propulsion Elements Ninth Edition</source>
    <publisher-name>John Wiley and Sons Inc</publisher-name>
    <publisher-loc>Canada</publisher-loc>
    <year>2017</year>
    <comment>[Book]</comment>
  </element-citation>
</ref>

<ref id="ref26">
  <element-citation publication-type="web">
    <person-group person-group-type="author">
      <name><surname>United States Environmental Protection Agency</surname><given-names></given-names></name>
    </person-group>
    <article-title>Contaminant Perchlorate Fact Sheet</article-title>
    <source>https://epa.gov</source>
    <year>2014</year>
    <comment>[Web]</comment>
  </element-citation>
</ref>

<ref id="ref27">
  <element-citation publication-type="book">
    <person-group person-group-type="author">
      <name><surname>Urbanski</surname><given-names>T.</given-names></name>
    </person-group>
    <source>Chemistry and Technology of Explosives</source>
    <publisher-name>Pergamon Press</publisher-name>
    <publisher-loc>Warszawa</publisher-loc>
    <year>1985</year>
    <comment>[Book]</comment>
  </element-citation>
</ref>

<ref id="ref28">
  <element-citation publication-type="journal">
    <person-group person-group-type="author">
      <name><surname>Yang</surname><given-names>S.</given-names></name>
      <name><surname>Xie</surname><given-names>K.</given-names></name>
      <name><surname>Wang</surname><given-names>J.</given-names></name>
      <!-- Others omitted -->
    </person-group>
    <article-title>Enhancing RDX Thermal Decomposition in Al@RDX Composite with Co Transition Metal Interfacial Layer</article-title>
    <source>Journal of Aerospace</source>
    <year>2024</year>
    <volume>11</volume>
    <issue>81</issue>
    <fpage>1</fpage>
    <lpage>12</lpage>
    <comment>[Journal]</comment>
  </element-citation>
</ref>

</ref-list>
</sec>
</body>
</article>
