NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Aerospace vehicle separation mechanisms selection, design, and use considerationsThe principal types of separation systems and mechanisms used in spacecraft are described and compared. Important parameters to be considered in tradeoff studies are discussed. Several examples of successful applications and failures and the lessons learned from them are discussed.
Document ID
19720005745
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Gluckman, I. B. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Publication Information
Publication: NASA. Goddard Space Flight Center 5th Aerospace Mech. Symp.
Subject Category
Space Vehicles
Accession Number
72N13394
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitle19720005742Collected WorksFifth Aerospace Mechanisms SymposiumN72-13391 04-15Collected Works
No Preview Available