Publication Date:
2019-07-13
Description:
Shock tube facility with high explosive driver for reentry flow conditions simulation of manned planetary flights
Keywords:
FACILITIES, RESEARCH, AND SUPPORT
Type:
U. OF TORONTO, AMERICAN PHYSICAL SOCIETY, U. S. AIR FORCE OFFICE OF SCIENTIFIC RESEARCH, CANADIAN ASSN. OF PHYSICISTS, CANADIAN AERONAUTICS AND SPACE INST., DEUTSCHE PHYSIKALISCHE GESELLSCHAFT, AND; Jun 23, 1969 - Jun 25, 1969; TORONTO; CANADA
Format:
text
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