Paper
15 November 1993 High-altitude shock-layer ultraviolet emissions measured using highly elliptical orbits
Deborah A. Levin, L. Carl Howlett, Leonard H. Caveny, David M. Mann
Author Affiliations +
Abstract
Predicting emissions under rarified flow conditions remains a challenge. Two rocket experiments (at 3.5 and 5 km/s) obtained the UV data under flight conditions using onboard instruments; the greatest discrepancies in the predictions occurred at the higher altitudes. An additional experiment is being planned to extend the velocity to 7 to 8 km/sec using instrumentation onboard a small satellite with a highly elliptical orbit. Scanning spectrometers and photometers will observe the periodic bow shock interactions. The periodic bow shock re- immersion to low altitudes (200 to 120 km) coupled to the orbital decay of the satellite, provide an opportunity to progressively map a broad region of rarified aerodynamics. The paper discusses the flight regime of the planned experiment, provides examples of the anticipated phenomena and calculations, and gives an indication of the preliminary sets of instruments and measurements planned.
© (1993) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Deborah A. Levin, L. Carl Howlett, Leonard H. Caveny, and David M. Mann "High-altitude shock-layer ultraviolet emissions measured using highly elliptical orbits", Proc. SPIE 1952, Surveillance Technologies and Imaging Components, (15 November 1993); https://doi.org/10.1117/12.161423
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KEYWORDS
Ultraviolet radiation

Satellites

Data modeling

Nose

Photometry

Monte Carlo methods

Rockets

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