NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

The auto‑search feature has been disabled based on user feedback. Enter a search term/phrase and click “Search” to begin.

Back to Results
Study of direct-return rendezvous trajectories using constant-thrust engines and rendezvous or maneuvering thrustersEffect of using two separate engines in lunar lander for direct-return rendezvous with vehicle
Document ID
19650026352
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Fletcher, H. S. (NASA Langley Research Center Hampton, VA, United States)
Williams, J. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1965
Subject Category
Space Sciences
Report/Patent Number
NASA-TN-D-3019
Report Number: NASA-TN-D-3019
Accession Number
65N35953
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LUNAR LANDING
RENDEZVOUS SPACECRAFT
ROCKET ENGINE

Related Records

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