A 20k payload launch vehicle fast track development concept using an RD-180 engine and a Centaur upper stage
By: compiled by R. Toelle.
Contributors: George C. Marshall Space Flight Center.
Series: NASA technical memorandum -- 108475.
Publisher: National Aeronautics and Space Administration, Marshall Space Flight Center; National Technical Information Service, distributor
Published: 1995
Place of publication: Marshall Space Flight Center, Ala; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamic configurations.; Centaur launch vehicle.; Concurrent engineering.; Launch vehicle configurations.; Liquid propellant rocket engines.; Payloads.; Upper stage rocket engines.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0410-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.