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Study on partially reusable launch system and flight demonstrator concept
- Source :
- 宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:宇宙輸送系基盤技術 = JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Space Transportation Systems. :21-24
- Publication Year :
- 2006
- Publisher :
- 宇宙航空研究開発機構, 2006.
-
Abstract
- This paper describes a summary of a conceptual study on a two-stage partially reusable launch vehicle system. The second stage is a conventional expendable vehicle while the first stage is reusable and glides back to a launch site after a powered turnaround maneuver. To realize such a system, several new technologies must be developed and demonstrated. The paper also summarizes the results of a design study on a flight demonstrator for the new technologies. This flight demonstrator is designated as RAFLEX (Reliable Ascent Flight Experiment).<br />資料番号: AA0049056004<br />レポート番号: JAXA-SP-05-010
Details
- Language :
- Japanese
- ISSN :
- 1349113X
- Database :
- OpenAIRE
- Journal :
- 宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:宇宙輸送系基盤技術 = JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Space Transportation Systems
- Accession number :
- edsair.jairo.........307640f04045e155bfdfbcaf8b498c6c