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HEAT AND MASS-TRANSFER CHARACTERISTICS OF AN AXIAL-FLOW LIQUID-CORE NUCLEAR ROCKET EMPLOYING RADIATION HEAT TRANSFER

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BookPublisher: Nasa, Washington, D.C. 1967Description: 46.DDC classification: NASA | TN D-4127

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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-4127 (Browse shelf)	Not for loan		TR14930

Total holds: 0

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Previous	NASA TN D-4124 BUCKLING OF A PRESSURIZED TOROIDAL RING UNDER UNIFORM EXTERNAL LOADING	NASA TN D-4125 EFFECT OF CANARDS IN REDUCING LAUNCH VEHICLE FLIGHT LOADS	NASA TN D-4126 TECHNICAL HISTORY OF THE ENVIRONMENTAL CONTROL SYSTEM FOR PROJECT MERCURY	NASA TN D-4127 HEAT AND MASS-TRANSFER CHARACTERISTICS OF AN AXIAL-FLOW LIQUID-CORE NUCLEAR ROCKET EMPLOYING RADIATION HEAT TRANSFER	NASA TN D-4128 STUDIES OF AIRFRAME--PROPULSION-SYSTEM INTEGRATION FOR MACH 6 CRUISE VEHICLES	NASA TN D-4129 TRANSITION FIXING FOR HYPERSONIC FLOW	NASA TN D-4130 AERODYNAMIC HEATING IN THE VICINITY OF CORNERS AT HYPERSONIC SPEEDS	Next

Bound With Nasa Tn D-4121-26,4128-30

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