NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Propulsion needs for lunar/Mars missionsViewgraphs on propulsion needs for lunar/Mars missions are presented. Topics covered include: lunar mission profile; lunar transfer vehicle/lunar excursion vehicle; launch vehicles for lunar missions; lunar outpost; Mars transfer operations; Mars mission vehicle in low earth orbit (LEO); mission vehicle commonality; mass comparison for reference missions; advanced propulsion; propulsion option size comparison; Mars transfer vehicle (MTV) propulsion option weights for mission favorable opportunities; propulsion options comparison; Mars transportation architecture options; tanker options for fully reusable systems; NTR 900 Isp staged tanks and engines; fully reusable cryogenic aerobraked system; NEP operated from high orbit; and nuclear safe orbit considerations.
Document ID
19930018609
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Woodcock, Gordon R.
(Boeing Aerospace and Electronics Co. Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1990
Publication Information
Publication: NASA, Washington, Technology for Space Station Evolution. Volume 3: EVA(Manned Systems)Fluid Management System
Subject Category
Spacecraft Propulsion And Power
Accession Number
93N27798
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available