Rocket Engine Systems for Hydrocarbon Fuels

机译：碳氢燃料火箭发动机系统

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Recent investigations into the use of non-toxic propellants for launcher propulsion show the potential to satisfy the market's performance and cost requirements. The main expected advantages are reduced handling effort and reduced safety precautions.rnSystem studies to identify the best non-toxic propellants have been performed. The chamber cooling performance was assessed regarding limitations by propellant dissociation and coking. Advantageous propulsion system configurations were investigated.rnMajor applications seen today are expendable liquid boosters, and reusable liquid flyback boosters. Booster concepts have been investigated for various non-toxic propellant and engine system combinations. Dimensions and performance are compared.

机译：最近对使用无毒推进剂进行发射器推进的研究表明，有潜力满足市场的性能和成本要求。预期的主要优点是减少了工作量并减少了安全预防措施。已经进行了系统研究，以确定最佳的无毒推进剂。通过推进剂离解和结焦来评估舱室冷却性能的局限性。研究了有利的推进系统配置。今天看到的主要应用是消耗性液体助推器和可重复使用的液体反激式助推器。已经针对各种无毒推进剂和发动机系统组合研究了助推器概念。比较尺寸和性能。

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来源
《1st International conference on green propellant for space propulsion》|2001年|p.1-8|共8页
会议地点 Noordwijk(NL)
作者
A. G?tz; C. M?ding; P. Philipp; D. Haeseler; G. Langel;
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作者单位

Astrium GmbH, Space Infrastructure Division, 81663 Munich, Germany Andreas.Goetz@astrium-space.com;

rnAstrium GmbH, Space Infrastructure Division, 81663 Munich, Germany;

rnAstrium GmbH, Space Infrastructure Division, 81663 Munich, Germany;

rnAstrium GmbH, Space Infrastructure Division, 81663 Munich, Germany Dietrich.Haeseler@astrium-space.com;

rnAstrium GmbH, Space Infrastructure Division, 81663 Munich, Germany Guenter.Langel@astrium-space.com;

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原文格式 PDF
正文语种 eng
中图分类空气动力学;
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3. Flow and thermal analyses of supercritical hydrocarbon fuel in curved regenerative cooling channel around cavity in rocket based combined cycle engine [J] . Jing Tingting, He Guoqiang, Li Wenqiang, Applied thermal engineering: Design, processes, equipment, economics . 2018,第期

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4. Rocket Engine Systems for Hydrocarbon Fuels [C] . A. G?tz, C. M?ding, P. Philipp, International conference on green propellant for space propulsion . 2001

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Rocket Engine Systems for Hydrocarbon Fuels

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