Optimal control theory determination of feasible return-to-launch-site aborts for the HL-20 personnel launch system vehicle
By: Kevin E. Dutton.
Contributors: Langley Research Center.
Series: NASA technical paper -- 3449.; NASA technical paper -- 3449.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1994
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Space vehicles -- Attitude control systems.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 94-0821-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.