TRAJECTORY OPTIMIZATION BY A DIRECT DESCENT PROCESS.
By: Fogarty,L E.
Contributor(s): Howe,R M.
Material type: BookPublisher: Nasa, Washington, D.C. Description: 36.DDC classification: NASA | CR-1070Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
---|---|---|---|---|---|---|---|
Technical Report | PK Kelkar Library, IIT Kanpur | General Stacks | NASA CR-1070 (Browse shelf) | Not for loan | TR11533 |
Total holds: 0
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NASA CR-1065 AN ANALYSIS OF THE COUPLED CHEMICALLY REACTING BOUNDARY LAYER AND CHARRING ABLATOR | NASA CR1067 INFRARED RADIOMETRIC STRESS INSTRUMENTATION APPLICATION RANGE STUDY. | NASA CR-1069 LUNAR ORBITER III. | NASA CR-1070 TRAJECTORY OPTIMIZATION BY A DIRECT DESCENT PROCESS. | NASA CR-1072 PLASMA BOUNDARY INTERACTIONS-II | NASA CR-1073 CRYOGENIC MAGNETOMETER DEVELOPMENT | NASA CR-1074 A LABORATORY SCALE MODEL TECHNIQUE FOR INVESTIGATING PNEUMATIC TIRE HYDROPLANING |
Bound With Nasa Cr-1066-69
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