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EXPERIMENTAL INVESTIGATION OF ROCKET-ENGINE ABLATIVE-MATERIALS PERFORMANCE AFTER POSTRUN COOLING AT ALTITUDE PRESSURES [NASA TN D-1726]

By: Rollbuhler, R. James.

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BookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington, D.C. National Aeronautics and Space Administration 1963Description: 29p.Subject(s): Material performance

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Item type	Current location	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D 1721-30	Not for loan		TR14338

Total holds: 0

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Previous	Lunar landing propulsion considerations [NASA TN D-1723]	CALIBRATIONS AND COMPARISONS OF PRESSURE-TYPE AIRSPEED-ALTITUDE SYSTEMS OF THE X-15 AIRPLANE FROM SUBSONIC TO HIGH SUPERSONIC SPEEDS [NASA TN D-1724]	TECHNIQUES USED TO MEASURE THE HYDRAULIC CHARACTERISTICS OF THE NASA PLUM BROOK REACTOR [NASA TN D-1725]	EXPERIMENTAL INVESTIGATION OF ROCKET-ENGINE ABLATIVE-MATERIALS PERFORMANCE AFTER POSTRUN COOLING AT ALTITUDE PRESSURES [NASA TN D-1726]	Experimental evaluation of liquid fluorine system components [NASA TN D-1727]	Rate of liquid jet breakup by a transverse shock wave [NASA TN D-1728]	CALIBRATION OF THERMAL-CONDUCTIVITY VACUUM GAGE IN THE RANGE OF 10 TO THE POWER OF MINUS 4 TO 1 TORR BY MEANS OF A VOLUME-RATIO CALIBRATION SYSTEM [NASA TN D-1729]	Next

Bound With NASA TN D 1721-30

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