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EFFECTS OF STEADY-STATE ACCELERATION ON COMBUSTION CHARACTERISTICS OF AN ALUMINIZED COMPOSITE SOLID PROPELLANT.

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BookPublisher: Nasa, Washington, D.C. 1968Description: 41.DDC classification: NASA | TN D-4914

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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-4914 (Browse shelf)	Not for loan		TR11374

Total holds: 0

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Previous	NASA TN D-490 THE ORIGIN OF TEKTITES	NASA TN D-4912 FEASIBILITY OF PRODUCING DISPERSION STRENGTHENED CHROMIUM BY BALL-MILLING IN HYDROGEN HALIDES.	NASA TN D-4913 CALCULATION OF FUEL LOSS FROM VENTED NUCLEAR FUEL ELEMENTS FOR SPACE POWER REACTORS.	NASA TN D-4914 EFFECTS OF STEADY-STATE ACCELERATION ON COMBUSTION CHARACTERISTICS OF AN ALUMINIZED COMPOSITE SOLID PROPELLANT.	NASA TN D-4915 LUNAR SURFACE TRNSMISSION LOSS FOR THE APOLLO ASTRONAUT.	NASA TN D-4916 POSTFLIGHT OPTICAL EVALUATION OF THE RIGHT-HAND AND LEFT-HAND WINDOWS OF GEMINI MISSIONS IV,V,VI, AND VII.	NASA TN D-4917 COMPUTE--A TIME-SHARING DESK CALCULATOR PROGRAM.	Next

Bound With Nasa Tn D-4911-13,4915-20

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