Results 91 to 100 of about 7,250 (196)
Hybrid Propulsion Technology Program [PDF]
Future launch systems of the United States will require improvements in booster safety, reliability, and cost. In order to increase payload capabilities, performance improvements are also desirable.
Holzman, A. L., Jensen, G. E.
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Journal of Aerospace Technology and Management, 2012 Rockets are powered by composite solid propellant, which is a heterogeneous system consisting of solid oxidizer and metallic fuel dispersed in a polymeric fuel binder matrix.
Praveen Prakash Singh +5 more
doaj
Three-dimensional finite element analysis of acoustic instability of solid propellant rocket motors [PDF]
A three dimensional finite element solution of the acoustic vibration problem in a solid propellant rocket motor is presented. The solution yields the natural circular frequencies of vibration and the corresponding acoustic pressure mode shapes ...
Hackett, R. M., Juruf, R. S.
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Performance of rocket nozzle materials with several solid propellants [PDF]
Erosion resistance and thermal stress cracking tests of rocket nozzle materials with solid ...
Freche, J. C. +2 more
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Solid rocket motor internal insulation [PDF]
Internal insulation in a solid rocket motor is defined as a layer of heat barrier material placed between the internal surface of the case propellant.
Keller, R. B., Jr., Twichell, S. E.
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Compatibility of grain-stabilized platinum with candidate propellants for resistojets [PDF]
Resistojets are candidates for space station auxiliary propulsion, and should be characterized by both long life and multipropellant operations, requirements limited by available materials.
Grisnik, S. P., Whalen, M. V.
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Launch Vehicle Description [PDF]
, 1970 The Thorad-Agena is a two-stage launch vehicle consisting of a Thorad first-stage and an Agena second-stage, connected by a booster adapter. The composite vehicle, including the shroud and the booster adapter, is about 33 meters (109 ft) long.
Coffey, E. E., Geye, R. P.
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Hybrid Propulsion Technology Program, phase 1. Volume 1: Executive summary [PDF]
The study program was contracted to evaluate concepts of hybrid propulsion, select the most optimum, and prepare a conceptual design package. Further, this study required preparation of a technology definition package to identify hybrid propulsion ...
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CLASSIFICATION OF SELF-PROPELLED GRAIN CLEANING MACHINES
Vestnik Altajskogo gosudarstvennogo agrarnogo universiteta, 2022 S.V. Lekanov, N.I. Strikunov
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An evaluation of aft-end ignition for solid propellant rocket motors [PDF]
Performance evaluation of solid propellant rocket motor ignition to determine igniter design and parameters to avoid ...
Fitch, R. E. +2 more
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