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Analysis of thermal-protection system for space-vehicle cryogenic-propellant tanks

By: George R. Smolak.

Contributor(s): Lewis E. Wallner.

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BookPublisher: DDC classification: NASA | TR R-130 -

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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 TR R-130 - (Browse shelf)	Not for loan		TR10289

Total holds: 0

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Previous	NASA TR R-127 - Tables of aerodynamic coefficients obtained from developed newtonian expression for complete and partial conic and spheric bodies at combind angles of attack and sideslip with some comparisons with	NASA TR R-128 - Study of an automatic system for control of the terminal phase of satellite rendezvous	NASA TR R-129 - Theoretical study of the torques induced by a magnetic field on rotating cylinders and spinning thin-wall cones,cone frustums,and general body of revolution	NASA TR R-130 - Analysis of thermal-protection system for space-vehicle cryogenic-propellant tanks	NASA TR R-137 - USE OF AN INERTIA SPHERE TO DAMP THE ANGULAR MOTIONS OF SPINNING SPACE VEHICLES	NASA TR R-138 - PROPAGATION OF PLANE ACOUSTIC WAVES IN A RADIATING GAS	NASA TR R-139 - THEORY OF INDUCED LIFT AND MINIMUM INDUCED DRAG OF NONPLANAR LIFTING SYSTEMS	Next

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