Preliminary vibration, acoustic, and shock design and test criteria for components on the lightweight external tank (LWT)/

Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Branch, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Systems Dynamics Laboratory U.S.
Format: Book
Language:English
Published: Washington, D.C.: National Aeronautics and Space Administration, Scientific and technical Information Branch, 1981
Series:NASA reference publication 1074
Subjects:
LEADER 01187nam a2200229 a 4500
001 785230
005 20171111231155.0
008 050119s1981 gr r f000 0 eng d
040 |a GR-KoDPT  |b gre  |e AACR2 
050 |a TL910  |b .P73 
082 0 |2 19  |a 629.47/1 
245 0 0 |a Preliminary vibration, acoustic, and shock design and test criteria for components on the lightweight external tank (LWT)/  |c Staff of Systems Dynamics Laboratory, George C. Marshall Space Flight Center 
260 |a Washington, D.C.:  |b National Aeronautics and Space Administration, Scientific and technical Information Branch,  |c 1981 
300 |a v, 315 σ. :  |b εικ. ;  |c 27 εκ. 
490 0 |a NASA reference publication  |v 1074 
500 |a Περιέχει ευρετήριο 
650 0 |a Space vehicles  |x Vibration 
650 0 |a Space vehicles  |x Testing 
710 |a United States  |b National Aeronautics and Space Administration  |b Scientific and Technical Information Branch 
710 0 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Branch 
710 2 |a Systems Dynamics Laboratory U.S. 
952 |a GR-KoDPT  |b 59cc2d4b6c5ad13446fa78e8  |c 998a  |d 945l  |e TL 521 .3  |t 1  |x m  |z Books