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High temperature antenna development for space shuttle, volume 1Design concepts for high temperature flush mounted Space Shuttle Orbiter antenna systems are discussed. The design concepts include antenna systems for VHF, L-band, S-band, C-band and Ku-band frequencies. The S-band antenna system design was completed and test hardware fabricated. It was then subjected to electrical and thermal testing to establish design requirements and determine reuse capabilities. The thermal tests consisted of applying ten high temperature cycles simulating the Orbiter entry heating environment in an arc tunnel plasma facility and observing the temperature distributions. Radiation pattern and impedance measurements before and after high temperature exposure were used to evaluated the antenna systems performance. Alternate window design concepts are considered. Layout drawings, supported by thermal and strength analyses, are given for each of the antenna system designs. The results of the electrical and thermal testing of the S-band antenna system are given.
Document ID
19740004409
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kuhlman, E. A.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Date Acquired
September 3, 2013
Publication Date
July 30, 1973
Subject Category
Space Vehicles
Report/Patent Number
MDC-E0896-VOL-1
NASA-CR-134136
Report Number: MDC-E0896-VOL-1
Report Number: NASA-CR-134136
Accession Number
74N12522
Funding Number(s)
CONTRACT_GRANT: NAS9-13004
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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