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NASA TM [X-100] : COMPARISON OF ROCKET PERFORMANCE USING EXHAUST DIFFUSER AND CONVENTIONAL TECHNIQUES FOR ALTITUDE SIMULATION

By: Sivo, Joseph N.

Contributor(s): Peters, Daniel J.

Series: NASA Technical Memorandum. Publisher: Nasa, Washington, D.C. 1961Description: 17p.Subject(s): Aerodynamics

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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 TM X-100	Not for loan		TR9396

Total holds: 0

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Previous	THERMAL RADIATION ABSORPTANCE AND VACUUM OUTGASSING CHARACTERISTICS OF SEVERAL METALLIC AND COATED SURFACES	FRICTION, WEAR, AND ADHESION CHARACTERISTICS OF TITANIUM-ALUMINUM ALLOYS IN VACUUM	NASA TM [X-786]	NASA TM [X-100]	NASA Technical Note: INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF A HYPERSONIC TRANSPORT MODEL AT MACH NUMBERS TO 6	NASA Technical Note: COMPARISONS OF TURBULENT-BOUNDARY-LAYER MEASUREMENTS AT MACH NUMBER 19.5 WITH THEORY AND AN ASSESSMENT OF PROBE ERRORS	NASA Technical Note: DYNAMIC AND STATIC WIND-TUNNEL TESTS OF A FLOW-DIRECTION VANE	Next

NASA Technical Memorandum X-71;72;75;83;85;86;89;92;100
Bounded Volumes Accession No. 102471; Contents: TR9389-96

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