NASA NTRS · 19810016600
Augmented orbiter heat rejection study
Abstract
Spacecraft radiator concepts are presented that relieve attitude restrictions required by the shuttle orbiter space radiator for baseline and extended capability STS missions. Cost effective heat rejection kits are considered which add additional capability in the form of attached spacelab radiators or a deployable radiator module.
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Hixon, C. W.. 1981-02-18. Augmented orbiter heat rejection study. https://ntrs.nasa.gov/citations/19810016600
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