Realization of an Eco-Friendly Solid Propellant Based on HIPB-HMX-AP System for Launch Vehicle Aplications

Rm. Muthiah; T. L. Varghese; S. S. Rao

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Realization of an Eco-Friendly Solid Propellant Based on HIPB-HMX-AP System for Launch Vehicle Aplications

机译：基于HIPB-HMX-AP系统的运载火箭应用生态友好型固体推进剂的实现

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摘要

An eco-friendly solid loaded HTPB propellant with improved energetics has been realized in small scale by incorporating 10-20% by weight of a high energy material namely, HMX.

机译：通过掺入10-20％重量的高能材料即HMX，已实现了小规模的，具有改善的能量学特性的环保型固体HTPB推进剂。

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《Propellants, Explosives, Pyrotechnics》 |1998年第2期|共4页
作者
Rm. Muthiah; T. L. Varghese; S. S. Rao;
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正文语种 eng
中图分类爆炸物工业、火柴工业;
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1. Realization of an Eco-Friendly Solid Propellant Based on HIPB-HMX-AP System for Launch Vehicle Aplications [J] . Rm. Muthiah, T. L. Varghese, S. S. Rao Propellants, Explosives, Pyrotechnics . 1998,第2期

机译：基于HIPB-HMX-AP系统的运载火箭应用生态友好型固体推进剂的实现
2. Multidisciplinary design optimization of a small solid propellant launch vehicle using system sensitivity analysis [J] . Jahangir Jodei, Masoud Ebrahimi, Jafar Roshanian Structural and Multidisciplinary Optimization . 2009,第1期

机译：基于系统灵敏度分析的小型固体推进剂运载火箭多学科设计优化
3. Multidisciplinary design optimization of a small solid propellant launch vehicle using system sensitivity analysis [J] . Jodei J, Ebrahimi M, Roshanian J Structural and multidisciplinary optimization . 2009,第1期

机译：基于系统灵敏度分析的小型固体推进剂运载火箭多学科设计优化
4. THE DIAMANT-A LAUNCH VEHICLE FIRST STAGE PROPULSION SYSTEM: A IIQUID-PROPELLANT ENGINE FITTED WITH A SOLID-PROPELLANT GAS GENERATOR [C] . Christophe ROTHMUND International astronautical congress;IAC 2009 . 2009

机译：DIAMANT-A发射车第一阶段推进系统：装有固体推进剂气体发生器的液体推进剂发动机
5. Experimental investigation and CFD simulation of active damping mechanism for propellant slosh in spacecraft launch systems [D] . Leuva, Dhawal 2011

机译：航天器发射系统推进剂晃荡主动阻尼机构的实验研究和CFD仿真
6. Fabrication of Eco-Friendly Solid-State Symmetric Ultracapacitor Device Based on Co-Doped PANI/GO Composite [O] . Hajera Gul, Anwar-ul-Haq Ali Shah, Salma Bilal 2019

机译：共掺杂PANI / GO复合材料的环保型固态对称超级电容器的制作
7. Launch Vehicle Performance with Solid Particle Feed Systems for Atomic Propellants [O] . Palaszewski, Bryan 1998

机译：带有固体推进剂的原子推进剂的运载火箭性能
8. Launch Vehicle Performance with Solid Particle Feed Systems for Atomic Propellants [R] . Palaszewski, B. 1998

机译：使用固体颗粒进料系统为原子推进剂发射车辆性能

Realization of an Eco-Friendly Solid Propellant Based on HIPB-HMX-AP System for Launch Vehicle Aplications

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