NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Orbiter entry trajectory control. 1 - High speed entry phaseDrag control method for space shuttle orbiter entry trajectory guidance
Document ID
19710016595
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mc Namara, J. (Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
August 6, 2013
Publication Date
April 1, 1971
Publication Information
Publication: NASA, WASHINGTON NASA SPACE SHUTTLE TECHNOL. CONF., VOL. 1 APR. 1971
Subject Category
Space Vehicles
Accession Number
71N26071
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available