Conceptual design of the LE-7-based reusable launch systems
- Author(s):
- Nakajima, M. ( Tohoku University, Sendai, Japan )
- Mizobata, K. ( Tohoku University, Sendai, Japan )
- Sawada, K. ( Tohoku University, Sendai, Japan )
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 1998
- Pub. Year:
- 1998
- No.:
- 98-0304
- Paper no.:
- 98-0304
- Page(from):
- 1
- Page(to):
- 11
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
Technical Paper
"Systems Analysis of a Future Semi-Reusable Launcher, Based on a High Thrust Bleed Cycle Rocket Engine"
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
Technical Paper
A conceptual design for the attitude control and determination system for the Magnetosphere Imager spacecraft
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |