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
Optimal guidance from hyperbolic to circular orbitsSolution for minimum fuel guidance from hyperbolic to circular orbit
Document ID
19680027315
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Edelbaum, T. N. (Analytical Mechanics Associates, Inc. Cambridge, MA, United States)
Date Acquired
August 4, 2013
Publication Date
January 1, 1968
Publication Information
Publication: NASA. ELECTRON. RES. CENTER TRAJECTORY ANALYSIS AND GUIDANCE THEORY JAN. 1968
Subject Category
Space Sciences
Meeting Information
Meeting: COLLOQ. ON ADVANCED PROBL. AND METHODS FOR SPACE FLIGHT OPTIMIZATION
Location: LIEGE
Start Date: June 19, 1967
End Date: June 23, 1967
Accession Number
68N36787
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

IDRelationTitleCollected Works19680027313Collected WorksTrajectory Analysis and Guidance Theory Second Compilation of Papers, 1 Oct. 1966 - 1 Oct. 1967N68-36785 23-30Collected Works19680027313Collected WorksTrajectory Analysis and Guidance Theory Second Compilation of Papers, 1 Oct. 1966 - 1 Oct. 1967
No Preview Available