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The measurements of vehicle glow on the Space ShuttleFrom the combined data set of glow observations on STS-3, STS-4 and STS-5 some of the properties of the shuttle glow were observed. Comparison of the STS-3 (240 km) and STS-5 (305 km) photographs show that the intensity of the glow is about a factor of 3.5 brighter on the low altitude (STS-3) flight. The orbiter was purposely rotated about the x axis in an experiment on STS-5 to observe the dependence of the intensity on the angle of incidence between the spacecraft surface normal and the velocity vector. For a relatively large angle between the velocity vector and the surface normal there is an appreciable glow, provided the surface is not shadowed by some other spacecraft structure. As the angle becomes less the glow intensifies. The grating experiments (STS-4 photography only, STS-5 image intensifier photography) provided a preliminary low resolution spectra of the spacecraft glow. Accurate wavelength calibrations of the STS-5 instrument permitted measuring of the spectrum and intensity of the Earth's airglow.
Document ID
19830022238
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mende, S. B.
(Lockheed Research Lab. Palo Alto, Calif., United States)
Banks, P. M.
(Stanford Univ. Calif., United States)
Nobles, R.
(Lockheed Missiles and Space Co. Palo Alto, Calif., United States)
Garriott, O. K.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Hoffman, J.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 4, 2013
Publication Date
March 15, 1983
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:85360
LMSC-D940124
NASA-TM-85360
Report Number: NAS 1.15:85360
Report Number: LMSC-D940124
Report Number: NASA-TM-85360
Accession Number
83N30509
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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