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AERODYNAMIC LOAD DISTRIBUTIONS FOR THE PROJECT FIRE CONFIGURATIONS AT MACH NUMBERS FROM 0.25 TO 4.63

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BookPublisher: Nasa, Washington, D.C. Description: 29.DDC classification: NASA | TN D-2604

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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-2604 (Browse shelf)	Not for loan		TR10875

Total holds: 0

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Previous	NASA TN D-2601M MARS NONSTOP ROUND-TRIP TRAJECTORIES.	NASA TN D-2601S STRESS-INTENSITY FACTORS FOR SINGLE-EDGE-NOTCH SPECIMENS IN BENDING FOR COMBINED BENDING AND TENSION BY BOUNDARY COLLOCATION OF A STRESS FUCTION	NASA TN D-2601T THERMAL DESIGN AND THERMAL DATA ANALYSIS OF SA-5 PAYLOAD	NASA TN D-2604 AERODYNAMIC LOAD DISTRIBUTIONS FOR THE PROJECT FIRE CONFIGURATIONS AT MACH NUMBERS FROM 0.25 TO 4.63	NASA TN D-2607 STABILITY OF FOUR TITANIUM-ALLOY AND FOUR STAINLESS-STEEL SHEET MATERIALS AFTER EXPOSURES UP TO 22000 HOURS AT 550 DEGREE F (560 DEGREE K).	NASA TN D-2608 RADIATION MEASUREMENTS ON THE NINTH MERCURY-ATLAS MISSION (MA-9).	NASA TN D-262 URANIUM DIOXIDE COMPATIBILITY WITH REFRACTORY METALS, CARBIDES, BORIDES, NITRIDES, AND OXIDES BETWEEN 3500(DEGRE ) AND 5000(DEGRE) F	Next

Bound With Nasa Tn D-2601-2601s, 2601m-2601l

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