NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Assured crew return vehicleA return vehicle is disclosed for use in returning a crew to Earth from low earth orbit in a safe and relatively cost effective manner. The return vehicle comprises a cylindrically-shaped crew compartment attached to the large diameter of a conical heat shield having a spherically rounded nose. On-board inertial navigation and cold gas control systems are used together with a de-orbit propulsion system to effect a landing near a preferred site on the surface of the Earth. State vectors and attitude data are loaded from the attached orbiting craft just prior to separation of the return vehicle.
Document ID
19920012756
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Cerimele, Christopher J.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Ried, Robert C.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Peterson, Wayne L.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Zupp, George A., Jr.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Stagnaro, Michael J.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Ross, Brian P.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
August 15, 2013
Publication Date
November 12, 1991
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
Patent Number: NASA-CASE-MSC-21536-1
Patent Number: US-PATENT-5,064,151
Patent Application Number: US-PATENT-APPL-SN-458476
Accession Number
92N21999
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-MSC-21536-1|US-PATENT-5,064,151
Patent Application
US-PATENT-APPL-SN-458476
No Preview Available