최소 단어 이상 선택하여야 합니다.
최대 10 단어까지만 선택 가능합니다.
다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.
NTIS 바로가기Acta astronautica, v.159, 2019년, pp.578 - 583
Schmierer, Christian (Institute of Space Propulsion, German Aerospace Center (DLR)) , Kobald, Mario (Institute of Space Propulsion, German Aerospace Center (DLR)) , Tomilin, Konstantin (HyImpulse Technologies GmbH) , Fischer, Ulrich (HyImpulse Technologies GmbH) , Schlechtriem, Stefan (Institute of Space Propulsion, German Aerospace Center (DLR))
Abstract Increased demand for smallsat launch capabilities drives on the search for low-cost launch vehicles. Hybrid rocket technology has been pushed forward in the recent years and is now ready to meet the demand of this low-cost rocket development. With intrinsic safety and reliability the devel...
https://www.spaceintelreport.com/for-euroconsult-coming-decade-to-see-nearly-6x-increase-in-smallsat-launches-50-telecom/.
http://www.euroconsult-ec.com/13_November_2018.
2007 Fundamentals of Hybrid Rocket Combustion and Propulsion
Prog. Astronaut. Aeronaut. Marxman 15 485 1964 Fundamentals of hybrid boundary combustion
Zilliac 2006 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit Hybrid rocket fuel regression rate data and modeling
Greene 2005 Hydrogen Peroxide Accidents and Incidents: what We Can Learn from History
Takahashi 2017 31st ISTS Japan Essentially non-explosive propulsion paving a way for fail-safe space transportation
Larson 1996 32nd Joint Propulsion Conference and Exhibit High pressure combustion of cryogenic solid fuels for hybrid rockets
J. Propul. Power Karabeyoglu 18 3 610 2002 10.2514/2.5975 Combustion of liquefying hybrid propellants: Part 1, general theory
Kobald 2014 50th AIAA&ASME/SAE/ASEE Joint Propulsion Conference Evaluation of paraffin-based fuels for hybrid rocket engines
CEAS Space Journal Kobald 7 1 11 2015 10.1007/s12567-015-0076-2 Theoretical and experimental analysis of liquid layer instabilities in hybrid rocket engines
Petrarolo 2016 Space Propulsion Conference 2016 Proceedings Optical analysis of hybrid rocket combustion with decomposition methods
J. Propul. Power Kobald 33 5 1245 2017 10.2514/1.B36207 Viscosity and regression rate of liquefying hybrid rocket fuels
J. Spacecraft Rockets Kobald 55 2 484 2018 10.2514/1.A34035 Hybrid experimental rocket Stuttgart: a low-cost technology demonstrator
Karabeyoglu 2005 41st AIAA/ASME/SAE/ASEE Join Propulsion Conference and Exhibit Evaluation of homologous series of normal-alkanes as hybrid rocket fuels
Traudt 2017 68th IAC An overview on the turbopump roadmap for the LUMEN demonstrator engine and on the new turbine test facility
Hahn 2018 Space Propulsion Conference Cycle analysis and feasibility evaluation of pump fed hybrid propulsion system
Ytterskog 2018 15th International Conference on Space Operations One step further towards a European launch capability for small satellites - SmallSat Express
*원문 PDF 파일 및 링크정보가 존재하지 않을 경우 KISTI DDS 시스템에서 제공하는 원문복사서비스를 사용할 수 있습니다.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.