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., NASA technical paper -- 3449.|
|Contributions||Langley Research Center.|
|The Physical Object|
Case studies in educational auditing
house on Cherry street
My Own Countrys Time
Dictionary of the Cree language
Police communication systems
You and your operation.
Catalog of the William Ransom Hogan Jazz Archive
Business handbook on terrorism, security, and survival
Words by heart.
Readings in twentieth-century European history.
Cumulative report on rescissions and deferrals, June 1982
Have you Seen Jesus?