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
Constant-attitude thrust program optimization.Optimum thrust programming studies include comparison of constant and variable attitude thrust programs for Earth-Mars rendezvous
Document ID
19650053706
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Melbourne, W. G.
Sauer, C. G., Jr.
Date Acquired
August 2, 2013
Publication Date
August 1, 1965
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 63-420
Report Number: AIAA PAPER 63-420
Accession Number
65A36410
Distribution Limits
Public
Copyright
Other
Keywords
TRAJECTORY OPTIMIZATION
EARTH-MARS RENDEZVOUS TRAJECTORY
OPTIMUM THRUST PROGRAMMING

Available Downloads

There are no available downloads for this record.

Related Records

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