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Analysis of reentry into the White Sands Missile Range (WSMR) for the LifeSat missionThis study investigates the reentry of the LifeSat vehicles into the WSMR. The LifeSat mission consists of two reusable reentry satellites, each carrying a removable payload module, which scientists will use to study long-term effects of microgravity, Van Allen belt radiation, and galactic cosmic rays on living organisms. A series of missions is planned for both low-Earth circular orbits and highly elliptic orbits. To recover the payload module with the specimens intact, a soft parachute landing and recovery at the WSMR is planned. This analysis examines operational issues surrounding the reentry scenario to assess the feasibility of the reentry.
Document ID
19930015528
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hametz, M.
(Computer Sciences Corp. Lanham, MD., United States)
Roszman, L.
(Computer Sciences Corp. Lanham, MD., United States)
Snow, F.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Cooley, J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Publication Information
Publication: Flight Mechanics(Estimation Theory Symposium, 1992
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
93N24717
Funding Number(s)
CONTRACT_GRANT: NAS5-31500
Distribution Limits
Public
Copyright
Public Use Permitted.
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