含能材料
含能材料
함능재료
ENERGETIC MATERIALS
2014年
6期
852-856
,共5页
付小龙%樊学忠%毕福强%王晗%李宏岩%李吉祯%刘小刚
付小龍%樊學忠%畢福彊%王晗%李宏巖%李吉禎%劉小剛
부소룡%번학충%필복강%왕함%리굉암%리길정%류소강
应用化学%固体推进剂%硝基呋咱%能量特性%理论计算
應用化學%固體推進劑%硝基呋偺%能量特性%理論計算
응용화학%고체추진제%초기부찰%능량특성%이론계산
applied chemistry%solid propellant%nitrofurazan%energy characteristic%theory calculation
根据最小自由能法,采用 NASA-CEA软件,研究了六种硝基呋咱化合物:3-硝基呋咱( NF)、3,4-二硝基呋咱( DNF)、3-硝氨基-4-硝基呋咱(NNF)、3-硝氨基-4-硝基呋咱铵盐(ANNF)、3-硝氨基-4-硝基呋咱肼盐(HNNF)和3-硝氨基-4-硝基呋咱羟胺盐(HANNF)的能量特性。研究了硝基呋咱化合物含量对复合改性双基(CMDB)推进剂能量特性的影响和压强对硝基呋咱/CMDB推进剂能量特性的影响。结果表明,HANNF和HNNF单元推进剂的比冲高于RDX,分别为2744.8 N·s·kg-1和2802.2 N·s·kg-1。六种硝基呋咱化合物使 CMDB推进剂的比冲大幅提高,其中 HNNF 和 HANNF 使 CMDB 推进剂的比冲分别提高74.6 N·s·kg-1和91 N·s·kg-1。六种硝基呋咱/CMDB推进剂的比冲均随压强升高而增加。比冲受压强影响顺序为DNF>NNF>HANNF>ANNF>HNNF>NF。
根據最小自由能法,採用 NASA-CEA軟件,研究瞭六種硝基呋偺化閤物:3-硝基呋偺( NF)、3,4-二硝基呋偺( DNF)、3-硝氨基-4-硝基呋偺(NNF)、3-硝氨基-4-硝基呋偺銨鹽(ANNF)、3-硝氨基-4-硝基呋偺肼鹽(HNNF)和3-硝氨基-4-硝基呋偺羥胺鹽(HANNF)的能量特性。研究瞭硝基呋偺化閤物含量對複閤改性雙基(CMDB)推進劑能量特性的影響和壓彊對硝基呋偺/CMDB推進劑能量特性的影響。結果錶明,HANNF和HNNF單元推進劑的比遲高于RDX,分彆為2744.8 N·s·kg-1和2802.2 N·s·kg-1。六種硝基呋偺化閤物使 CMDB推進劑的比遲大幅提高,其中 HNNF 和 HANNF 使 CMDB 推進劑的比遲分彆提高74.6 N·s·kg-1和91 N·s·kg-1。六種硝基呋偺/CMDB推進劑的比遲均隨壓彊升高而增加。比遲受壓彊影響順序為DNF>NNF>HANNF>ANNF>HNNF>NF。
근거최소자유능법,채용 NASA-CEA연건,연구료륙충초기부찰화합물:3-초기부찰( NF)、3,4-이초기부찰( DNF)、3-초안기-4-초기부찰(NNF)、3-초안기-4-초기부찰안염(ANNF)、3-초안기-4-초기부찰정염(HNNF)화3-초안기-4-초기부찰간알염(HANNF)적능량특성。연구료초기부찰화합물함량대복합개성쌍기(CMDB)추진제능량특성적영향화압강대초기부찰/CMDB추진제능량특성적영향。결과표명,HANNF화HNNF단원추진제적비충고우RDX,분별위2744.8 N·s·kg-1화2802.2 N·s·kg-1。륙충초기부찰화합물사 CMDB추진제적비충대폭제고,기중 HNNF 화 HANNF 사 CMDB 추진제적비충분별제고74.6 N·s·kg-1화91 N·s·kg-1。륙충초기부찰/CMDB추진제적비충균수압강승고이증가。비충수압강영향순서위DNF>NNF>HANNF>ANNF>HNNF>NF。
Based on the minimum free energy method,the energy characteristics of six nitrofurazan compounds,3-nitrofurazan (NF),3,4-dinitrofurazan(DNF),3-nitrimino-4-nitrofurazan(NNF),3-nitramino-4-nitrofurazan ammonium salt(ANNF),3-niti-mino-4-nitrofurazan hydrazonium salt( HNNF)and 3-nitramino-4-nitrofurazan hydroxyl ammonium( HANNF),were studied by NASA- CEA software. Effects of the content of nitrofurazan compounds on the energy characteristics of CMDB propellants and effects of pressure on the energy characteristics of nitrofurazan /CMDB propellants were studied. Results show that the specific impulses of HANNF and HNNF monopropellants are 2744. 8 N·s·kg-1 and 2802. 2 N·s·kg-1 ,respectively,which are obviously higher than that of RDX. Six nitrofurazan compounds make the specific impulse of CMDB propellants increase substantially,in which HNNF and HANNF make the specific impulse of CMDB propellants increase by 74.6 N·s·kg-1 and 91 N·s·kg-1,respectively. The specific impulse for the six propellants increases with the increase of pressure. The order affecting the specific impulse by pres-sure is DNF>NNF>HANNF>ANNF>HNNF>NF.