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Preliminary subsystem designs for the Assured Crew Return Vehicle (ACRV)Described herein is a series of design studies concerning the Assured Crew Return Vehicle (ACRV). Study topics include a braking and landing system for the ACRV, ACRV growth options, and the design impacts of ACRV's role as a medical emergency vehicle. Four alternate designs are presented for the ACRV braking and landing system. Options presented include ballistic and lifting body reentries; the use of high-lift, high-payload aerodynamic decelerators, as well as conventional parachutes; landing systems designed for water landings, land landings or both; and an aerial recovery system. Uses of the ACRV or a similarly designed vehicle in several roles for possible future space missions are discussed, along with the required changes to the ACRV to allow it to perform these missions optimally. The impacts on the design of the ACRV due to its role as an emergency vehicle were studied and are presented here. This study included the design of a stretcher-like system to transport an ill or injured crewmember safely within the ACRV; a compilation of necessary medical equipment and decisions on how or where to store it; and recommendations about internal and external vehicle characteristics that will ease the transport of the ill or injured crewmember and allow for swift and easy ingress/egress of the vehicle.
Document ID
19910008835
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Date Acquired
September 6, 2013
Publication Date
November 1, 1990
Publication Information
Publication: USRA, Proceedings of the 6th Annual Summer Conference: NASA(USRA University Advanced Design Program
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
91N18148
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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