3 edition of Optimal control theory determination of feasible return-to-launch-site aborts for the HL-20 personnel launch system vehicle found in the catalog.
Optimal control theory determination of feasible return-to-launch-site aborts for the HL-20 personnel launch system vehicle
by National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor in Hampton, Va, [Springfield, Va
Written in English
|Statement||Kevin E. Dutton.|
|Series||NASA technical paper -- 3449.|
|Contributions||Langley Research Center.|
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