Throttling dynamic response of LH2 rocket engine for vertical landing rocket vehicle

Advances in the Astronautical Sciences

Volumn 96, Issue , 1997, Pages 229-240

  Naruo, Yoshihiro ^a   Inatani, Yoshifumi ^a   Morita, Yasuhiro ^a   Nakai, Shunichiro ^b   Mori, Hatsuo ^b  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b IHI CORPORATION   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0005692263     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (3)

1. Weeger, R. K., "SSTO Propulsion Design," AIAA-92-1384, 1992
2. Inatani, Y., Naruo, Y and Yamada, T., "A Concept of Reusable Sounding Rocket with Enhanced Maneuverability and Operability," Proc. 20th.International Symposium for Space Technology and Science, Gifu, 1996
3. Ikeda, T., et al. "LOX/LH2 Propulsion System for Launch Vehicle Upper Stage," Ishikawajimaharima Heavy Industry Technical Report No.1, vol.23, 1983