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Preliminary analysis of STS-2 entry flight dataA preliminary analysis of the data obtained during the entry of the STS-2 flight was completed. The stability and control derivatives from STS-2 were examined. Questions still remain throughout the flight envelope and the area below Mach 3 needs more study. With three controls operating in a high gain feedback system, it is difficult to separate the individual effects of each of the controls. Analysis of the aerothermal data shows that wing structural-temperature measurements are generally repeatable and consistent with the trajectories. The measured wing upper surface temperatures are in reasonable agreement with Dryden predictions but wing lower surface temperatures are higher than Dryden predictions. Heating and heat transfer models will be adjusted to improve the temperature prediction capability for future trajectories.
Document ID
19820014430
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Date Acquired
September 4, 2013
Publication Date
April 1, 1982
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-81371
NAS 1.15:81371
Report Number: NASA-TM-81371
Report Number: NAS 1.15:81371
Accession Number
82N22304
Funding Number(s)
PROJECT: RTOP 989-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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