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ANALYSIS OF ASYMMETRIC MASS ADDITION EFFECTS ON RE-ENTRY BODY FLOWFIELD AND AERODYNAMIC CHARACTERISTICS

Author(s):
Chrusciel, G.T. ( Lockheed Martin Missiles & Space )  
Publication title:
AIAA paper
Title of ser.:
AIAA Paper : Aerospace Sciences Meeting and Exhibit
Ser. no.:
1999
Pub. Year:
1999
No.:
99-0433
Paper no.:
99-0433
Page(from):
1
Page(to):
17
Pub. info.:
American Institute of Aeronautics and Astronautics
ISSN:
01463705
Language:
English
Call no.:
A07400
Type:
Technical Paper

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