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A design study of a regeneratively cooled nozzle for a tungsten water-moderated nuclear rocket system [NASA-TN-D-3771]

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BookSeries: National Aeronautics and Space Administration [NASA]. Publisher: Washington, D. C. NASA 1966Description: 32p.Subject(s): TungstenDDC classification: NASA | TN-D-3771

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	Reference	NASA TN-D-3771 (Browse shelf)	Not for loan		83105

Total holds: 0

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Previous	NASA TN D-4776 Performance and stability characteristics of nitrogen tetroxide-hydrazine combustors [NASA TN D-4776]	NASA TN-D-2477 Effects of gross changes in static directional stability on v/stol handling characteristics based on a flight investigation	NASA TN-D-3711 A method for the measurement of extremely feeble torques on massive bodies [NASA TN-D-3711]	NASA TN-D-3771 A design study of a regeneratively cooled nozzle for a tungsten water-moderated nuclear rocket system [NASA-TN-D-3771]	NASA TN-D-3772 Extrusion of 1/2-inch diameter and 3/8-inch diameter, thin-wall tungsten tubing using the floating-mandrel technique [NASA-TN-D-3772]	NASA TN-D-3773 Simulation of liquid-hydrogen turbine-type flowmeter calibrations using high-pressure gas [NASA-TN-D-3773]	NASA TN-D-3774 Dynamic model investigation of the rough-water landing characteristics of a spacecraft [NASA TN-D-3774]	Next

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