NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
CONSTANT ATTITUDE THRUST PROGRAM OPTIMIZATIONOptimum thrust programming studies include a comparison of constant and variable attitude thrust programs for an earth-mars rendezvous
Document ID
19630025672
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Melbourne, W. G.
Sauer, C. G., Jr.
Date Acquired
August 1, 2013
Publication Date
August 21, 1963
Subject Category
Space Radiation
Report/Patent Number
AIAA PAPER 63-420
Report Number: AIAA PAPER 63-420
Accession Number
63A21731
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other
Keywords
THRUST PROGRAMMING
TRAJECTORY
OPTIMUM THRUST PROGRAMMING
SPACECRAFT TRAJECTORY

Available Downloads

There are no available downloads for this record.

Related Records

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