Improvements in Re-usable Solid Rocket Motor Performance Predictions
Author : Brent Wiesenberg
Publisher :
Page : pages
File Size : 14,1 MB
Release : 2000
Category :
ISBN :
Author : Brent Wiesenberg
Publisher :
Page : pages
File Size : 14,1 MB
Release : 2000
Category :
ISBN :
Author : William H. Miller
Publisher :
Page : 124 pages
File Size : 21,94 MB
Release : 1971
Category : Solid propellant rockets
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Author : Roger Cook
Publisher :
Page : pages
File Size : 20,8 MB
Release : 1997
Category :
ISBN :
Author : Estats Units d'Amèrica. National Aeronautics and Space Administration. Space Vehicle Design Criteria (Chemical Propulsion)
Publisher :
Page : 106 pages
File Size : 23,87 MB
Release : 1971
Category :
ISBN :
Author : W. H. Miller
Publisher :
Page : 20 pages
File Size : 42,68 MB
Release : 1969
Category : Solid propellant rockets
ISBN :
Author : James E. Vint
Publisher :
Page : 38 pages
File Size : 10,74 MB
Release : 1968
Category :
ISBN :
A technique developed by the Rohm and Haas Company for specific impulse scaling has been adapted for use at the Air Force Rocket Propulsion Laboratory. The purpose of this technique is to predict specific impulse in large solid rocket motors based on data obtained in micromotors. As little as 2 pounds of propellant are required to obtain the data from which the prediction is made. The technique has been checked with a composite-modified-double-base propellant and a polybutadiene composite propellant. Within the limitations described, this technique can provide useful information concerning performance of a propellant in a large solid motor. Predictions, based on data obtained in micromotors, were within 0.6% of the delivered impulse in 6-pound motors and 70-pound BATES motors. (Author).
Author : Brent C. Wiesenberg
Publisher :
Page : 178 pages
File Size : 45,61 MB
Release : 1997
Category : Neural networks (Computer science)
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Author : Xin Wang
Publisher :
Page : 15 pages
File Size : 49,91 MB
Release : 1986
Category :
ISBN :
This article introduces two predictive algorithms for the performance of solid propellant rocket motor. The emphasis is on the introduction of Time-Space Algorithm. The authors proposed a general two-dimensional grain calculation procedure in order to conduct the grain calculations. Therefore, the predictive algorithms for performance introduced by this article show generality. A comprehensive computer program for the aforementioned method has been written and applied to calculating the performance of three different solid rocket motors. The calculated results are consistent with those derived from experimental data.
Author : Carlton L. Horine
Publisher :
Page : 96 pages
File Size : 30,54 MB
Release : 1971
Category : Solid propellant rockets
ISBN :
Author :
Publisher :
Page : 642 pages
File Size : 11,96 MB
Release : 2000
Category : Airplanes
ISBN :