Shuttle entry technology payloadsThe flight frequency of the Space Transportation System (STS) coupled with its large payload-carrying capability will provide an unprecedented opportunity for conducting aerothermodynamic/entry technology research. This STS research opportunity can be characterized into two distinct categories: (1) that research which will utilize the STS orbiter as the test vehicle, and (2) that research which will utilize a vehicle launched from the orbiter for entry. To date, on-going studies have defined experiments as well as the support systems required for the shuttle launched research program. The proposed Entry Technology Program will provide a flight data base from which accurate correlations can be performed relative to ground test and analysis data. These correlations will result in optimized designs for future flight systems.
Document ID
19760029925
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Siemers, P. M., III (NASA Langley Research Center Space Systems Div., Hampton, Va., United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Subject Category
Astronautics (General)
Report/Patent Number
AAS PAPER 75-251
Meeting Information
Meeting: Meeting on Space Shuttle Missions of the 80''s