Research activities to realize advanced space transportation system

15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 2008, Pages

  Fujii, Kenji ^a,b   Ishimoto, Shinji ^a,b  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b Space Transportation Mission Directorate ^*  (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

LAUNCH VEHICLES; MASS TRANSPORTATION; ROCKETS; SPACE FLIGHT; SPACE RESEARCH;

ADVANCED TECHNOLOGY; DESIGN TECHNOLOGIES; GLOBAL COMPETITIVENESS; JAPAN AEROSPACE EXPLORATION AGENCY; RESEARCH ACTIVITIES; RESEARCH AND DEVELOPMENT; SPACE TRANSPORTATION SYSTEM; TECHNOLOGICAL LIMIT;

RESEARCH AND DEVELOPMENT MANAGEMENT;

EID: 77958481881     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-2575     Document Type: Conference Paper

References (4)

1. Ishimoto, S. and Mori, T., "Study on a Two-Stage Partially Reusable Launch Vehicle as a Reference System," The 48th Space Sciences and Technology Conference Japan, 2A11, 4-6 November, pp. 656-61.
2. Minami, Y., Ishimoto, S., Mori, T., and Fujii, K., "Design Study on a Small-Sized Partially Reusable Launch System," AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies, AIAA 2005-3249, AIAA, 2005.
3. The Space Propulsion Synergy Team, "A Guide for the Design of Highly Reusable Space Transportation," http://science.ksc.nasa.gov/shuttle/ nexgen/Guide-HRST-Design/rlvgide.htm, NASA, August 29, 1997.
4. Fujii, K., Ishimoto, S., and Shimura, K., "Reliable Ascent Flight Experiment: RAFLEX," AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies, AIAA 2005-3349, AIAA, 2005.