介绍了代表目前运载火箭固体发动机材料技术水平的欧洲织女星(Vega)三级发动机和作为未来织女星和新一代运载火箭技术验证的Zefiro 40发动机以及日本Epsilon固体发动机的技术特点及其复合材料与工艺研究进展,结合我国运载火箭固体发动机材料的技术现状,提出发展建议.
参考文献
| [1] | GSLV launched successfully[J].Current Science: A Fortnightly Journal of Research,2001(10):1254-1256. |
| [2] | Stefano Bianchi .VEGA, the European small launcher: Development status, future perspectives, and applications[J].Acta astronautica,2008(1/4):416-427. |
| [3] | Didier Boury;Aude Copey;Philippe Cloutet.Large solid rocket motors for future european launcher[A].Atlanta,Georgia,2012 |
| [4] | Marco BIAGIONI;Maurizio CUTRONI;Philippe PASCAL.P80 FW SRM-new technologies for solid rocket motor-status of development[A].Fort Lauderdale,Florida,2004 |
| [5] | Gautronneau E;Cros C Ph.Pascal.Vega program-the P80 FW SRM nozzle[A].Fort Lauderdale,Florida,2004 |
| [6] | Gautronneau E;Boury D;Chevrollier A.P80 nozzle low cost technologies[A].,2006 |
| [7] | Michel Berdiyes;Martine Dauchier;Christophe Just.A new ablative material offering nozzle design breakthroughs[A].San Diego,California,2011 |
| [8] | Peake S L;Ellis R A;Broquere B.Update:sustainable carbonized rayon for solid rocket motor nozzles[A].Sacramento,California |
| [9] | Boury D;Bouvier F;Chevrollier A.C2b rayon source requalification for carbon phenolic nozzle insulators[A].San Diego,California,2011 |
| [10] | Angelone M;Mascanzoni F;Milana C.Technological and programmatic development of Zefiro 40 solid rocket motor[A].Atlanta,Georgia |
| [11] | Imoto T;Morita Y;Tokudome S.The development status of the epsilon launch vehicle[A].Kyoto,Japan,2012 |
| [12] | Tokudome S;Habu H;Ui K.Solid propulsion systems for epsilon launch vehicle[A].Atlanta,Georgia,2012 |
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