2002
DOI: 10.2514/2.5909
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Overview of the Development of Hydrazinium Nitroformate-Based Propellants

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Cited by 31 publications
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“…Trinitromethane (nitroform, 7 ) appears as the intermediate in the hydrazine nitroformate decomposition, which is a promising chlorine-free oxidant for the solid rocket fuel. Thermodynamic characteristics of nitroform and intermediates of its decomposition as well as the rate constants of elementary reactions are crucial for modeling the complex process of the hydrazine nitroformate combustion. , …”
Section: Introductionmentioning
confidence: 99%
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“…Trinitromethane (nitroform, 7 ) appears as the intermediate in the hydrazine nitroformate decomposition, which is a promising chlorine-free oxidant for the solid rocket fuel. Thermodynamic characteristics of nitroform and intermediates of its decomposition as well as the rate constants of elementary reactions are crucial for modeling the complex process of the hydrazine nitroformate combustion. , …”
Section: Introductionmentioning
confidence: 99%
“…18,20,21 Trinitromethane (nitroform, 7) appears as the intermediate in the hydrazine nitroformate decomposition, which is a promising chlorine-free oxidant for the solid rocket fuel. [23][24][25][26][27] Thermodynamic characteristics of nitroform and intermediates of its decomposition as well as the rate constants of elementary reactions are crucial for modeling the complex process of the hydrazine nitroformate combustion. 27,28 Although the nitroalkanes have been studied extensively, there is still some disagreement among the existing experimental thermodynamic data, especially on the formation enthalpy of these species.…”
Section: Introductionmentioning
confidence: 99%
“…The main criteria in the demand for an energetic oxidizer are high density, high enthalpy of formation, and high positive oxygen balance. Ammonium perchlorate (AP) is the most widely used oxidizer in composite (CP) and composite-modified double base (CMDB) rocket propellants. However, as the most popular oxidizer, AP has its own inherent disadvantage in the production of chlorine-rich combustion products (30%), which will cause environmental problems such as ozone depletion and acid rain. Energetic eco-friendly oxidizers ammonium dinitramide (ADN) and hydrazinium nitroformate (HNF) have entered in the domain of advanced propellant systems because they offer halogen-free propellant formulations. In comparison with ADN, HNF has certain advantages such as its simple synthetic route, higher melting point (b.p.) and lower hygroscopicity. , The synthesis of HNF involves a two-step process comprising the preparation of nitroform (NF) and its neutralization with hydrazine to form HNF (Scheme ).…”
Section: Introductionmentioning
confidence: 99%
“…For the first time, the HNF-based propellants were investigated in some detail in the 1960s, but the research program was terminated, primarily because of the low stability of this compound and hazardous methods of its synthesis. The interest in HNF was revived in the late 1970s when safe synthetic procedures and efficient stabilizers and binders were found. ,,,, …”
Section: Introductionmentioning
confidence: 99%