NEW DEVELOPMENTS ON ROCKET PROPULSION WITH GELLED PROPELLANTS

机译：凝胶推进剂在火箭推进方面的新进展

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Gelled propellant rocket motor (GRM) technology development started in Germany in 2000 as an activity of Bayern-Chemie (BC), the research institutes FhG-ICT and DLR-IRA and the BWB (now BAAINBw) that funded the activity on behalf of the German MoD. After two perfectly successful demonstration flights of a monopropellant GRM in December 2009 the program goes on to improve the performance and functional parameters. Based on the concept design for a kick stage / trajectory insert stage motor presented in 2011, this paper describes the progress achieved within the last two years and the impact on the performance of this system and other applications like first stage motors or attitude control systems.

机译：胶凝推进剂火箭发动机（GRM）技术的开发始于2000年德国的拜仁－化学（BC），研究机构FhG-ICT和DLR-IRA以及由BWB（现为BAAINBw）资助的这项活动。德国国防部。在2009年12月进行了两次成功的单推进剂GRM示范飞行之后，该计划继续改进性能和功能参数。基于2011年提出的反冲级/弹道级电机的概念设计，本文描述了过去两年中取得的进展以及对该系统和其他应用（如一级电机或姿态控制系统）性能的影响。

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《European rocket amp; balloon programmes and related research》|2013年|451-457|共7页
会议地点 Thun(CH)
作者
Karl Wieland Naumann; Juergen Ramsel; Konrad Schmid; Helmut Niedermaier; Pedro Caldas-Pinto; Albert Thumann;
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Bayern-Chemie GmbH, PO. Box 1131, D-84544 Aschau/Inn, Germany;

Bayern-Chemie GmbH, PO. Box 1131, D-84544 Aschau/Inn, Germany;

Bayern-Chemie GmbH, PO. Box 1131, D-84544 Aschau/Inn, Germany;

Bayern-Chemie GmbH, PO. Box 1131, D-84544 Aschau/Inn, Germany;

Bayern-Chemie GmbH, PO. Box 1131, D-84544 Aschau/Inn, Germany;

Bayern-Chemie GmbH, PO. Box 1131, D-84544 Aschau/Inn, Germany;

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专利

1. ADVANCED LIQUID AND GELLED PROPELLANTS FOR ROCKET AND RAMJET PROPULSION [J] . Helmut K. Ciezki, Michele Negri, Andreas Gernoth International journal of energetic materials and chemical propulsion . 2015,第2期

机译：用于火箭和RAMJET推进的高级液体和胶凝推进剂
2. Air gel - THE DEVELOPMENT AND TEST OF ROCKETS WITH THE NEW CLASS OF GELLED PROPELLANTS [J] . KARL WIELAND NAUMANN Aerospace Testing International . 2010,第6期

机译：气凝胶-新型胶凝推进剂对火箭的研制与试验
3. BASIC MATLAB SIMULATION OF ION PROPULSION ROCKET BY CHLORINE AS PROPELLANT VIA NEGATIVE ION PAIR THRUSTING [J] . A. KANNI RAJ International Journal of Engineering Science and Technology . 2019,第2期

机译：负离子对通过氯作为推进剂的离子推进火箭的基本MATLAB模拟
4. NEW DEVELOPMENTS ON ROCKET PROPULSION WITH GELLED PROPELLANTS [C] . Karl Wieland Naumann, Juergen Ramsel, Konrad Schmid, ESA symposium on European rocket balloon programmes and related research . 2013

机译：凝胶推进剂火箭推进剂的新发展
5. ACCELERATION EFFECTS IN SOLID PROPELLANT ROCKET MOTORS (PROPULSION). [D] . LANGHENRY, MARK THOMAS. 1985

机译：固体推进剂火箭发动机（推进力）的加速作用。
6. Examination of the liver in personnel working with liquid rocket propellant [O] . Palle Petersen, Erik Bredahl, Ove Lauritsen, 1970

机译：液体火箭推进剂工作人员的肝脏检查
7. Neki aspekti performansi raketnih goriva i pravci razvoja čvrstih raketnih goriva / Some aspects of rocket propellant performances and solid rocket propellant development tendencies [O] . Radun Jeremić 2004

机译：Neki aspekti performansi raketnih goriva i pravcirazvojačvrstihraketnihgoriva /火箭推进剂性能和固体火箭推进剂发展趋势的某些方面
8. Preliminary Assessment of Using Gelled and Hybrid Propellant Propulsion for VTOL/SSTO Launch Systems [R] . Palaszewski, B. , OLeary, R. , Pelaccio, D. G. 1998

机译：用于VTOL / ssTO发射系统的胶凝和混合推进剂推进的初步评估

NEW DEVELOPMENTS ON ROCKET PROPULSION WITH GELLED PROPELLANTS

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