Results 271 to 280 of about 61,097 (314)
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Hybrid rocket motor fuel studies
33rd Joint Propulsion Conference and Exhibit, 1997Results from four fuel characterization studies are reported. The first study was a premix (complete fuel except for curative) hold time determination which concluded that a full-scale 600-gal premix could be held for at least 3 weeks without any harmful degradation of the cured final fuel.
H. Weyland, H. Weyland
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Solid-Propellant Rocket Motors
2012The solid-propellant rocket motor brings the flight mission capability of high thrust delivery over a short duration. Design issues, such as tailoring the shape of the solid propellant grain (charge) to produce a desired thrust-time profile, are discussed in some detail in this chapter.
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1963
Abstract : This report concerns the use of W in solid propellant rocket motors and involves two main areas of interest. The first area, W erosion, is being studied under simulated exhaust conditions by means of a specially constructed plasma arc erosion apparatus. The second area deals with the effects of thermal shock on W and includes an experimental
DAVID A. BROWN, GERALD M. GORDON
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Abstract : This report concerns the use of W in solid propellant rocket motors and involves two main areas of interest. The first area, W erosion, is being studied under simulated exhaust conditions by means of a specially constructed plasma arc erosion apparatus. The second area deals with the effects of thermal shock on W and includes an experimental
DAVID A. BROWN, GERALD M. GORDON
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Interior Ballistics of Rocket Motors
Nature, 1961Rocket Propellant Handbook By Boris Kit and Douglas S. Evered. Pp. xiv + 354. (New York and London: The Macmillan Company, New York, 1960.) 12.50 dollars; 87s. 6d. Liquid Propellant Rockets By David Altman, James M. Carter, S. S. Penner and Martin Summerfield. (Prineeton Aeronautical Paperbacks, No. 1.) Pp. v + 189.
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SEGMENTED ROCKET MOTOR CASE PROGRAM
1962Abstract : This is an interim report on a research and development program directed toward design, development, fabrication, and testing of lightweight motor case segments, culminating in a design applicable to large (160- to 240- in. dia.) segmented solid propellant rocket motors.
T. R. JEFFUS, R. G. CARPENTER
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Hybrid rocket motor experiments
1985Aerospace ...
Timnat, Y.M. (author) +1 more
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Transient investigation of nozzle erosion in a long-time working hybrid rocket motor
Aerospace Science and Technology, 2021Guobiao Cai, Yuanjun Zhang
exaly

