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ORBITAL PAYLOAD REDUCTIONS RESULTING FROM BOOSTER AND TRAJECTORY MODIFICATIONS FOR RECOVERY OF A LARGE ROCKET BOOSTER

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BookPublisher: Nasa, Washington, D.C. 1961Description: 17.DDC classification: NASA | TN D-1143 -

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-1143 - (Browse shelf)	Not for loan		TR9577

Total holds: 0

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Previous	NASA TN D-1109 INVESTIGATION OF THE PERFORMANCE OF AN AXIAL-FLOW-PUMP STAGE DESIGNED BY THE BLADE-ELEMENT THEORY-BLADE-ELEMENT DATA	NASA TN D-1110 A PARAMETRIC STUDY OF THE THERMIONIC DIODE SYSTEM FOR LARGE NUCLEAR-ELECTRIC POWERPLANTS IN SPACE VEHICLES	NASA TN D-1142 - POINT RETURN FROM A LUNAR MISSION FOR A VEHICLE THAT MANEUVERS WITHIN THE EARTH'S ATMOSPHERE	NASA TN D-1143 - ORBITAL PAYLOAD REDUCTIONS RESULTING FROM BOOSTER AND TRAJECTORY MODIFICATIONS FOR RECOVERY OF A LARGE ROCKET BOOSTER	NASA TN D-1144 - AN ACCELERATED RESERVOIR LIGHT-GAS GUN	NASA TN D-1145 - ATMOSPHERE ENTRIES WITH VIHICLE LIFT-DRAG RATIO MODILATED TO LIMIT DECELERATION -VEHICLES WITH MAXIMUM LIFT-DRAG RATIO OF 0.52	NASA TN D-1146 - EFFECTS OF SURFACE RECOMBINATION ON HEAT TRANSFER TO BODIES IN A HIGH ENTHALPY STREAM OF PARTIALLY DISSOCIATED NITROGEN	Next

Bound With Nasa Tn D-1141-50

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