Zobrazeno 1 - 8
of 8
pro vyhledávání: '"E. M. Landsbaum"'
Autor:
E. M. Landsbaum
Publikováno v:
Journal of Propulsion and Power. 21:470-477
A solid-propellant rocket motor test that exhibited unexpected erosive burning led to an extensive literature review of the subject. A qualitative theory that explains why higher burning-rate propellants are less prone to erosive burning, why propell
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fcd4bdb8fbe918bf38ac9d88c12486ad
https://doi.org/10.2514/1.5234
https://doi.org/10.2514/1.5234
Autor:
E. M. Landsbaum
Publikováno v:
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a3cfe70c791c114d10aed522faa1e816
https://doi.org/10.2514/6.2003-4805
https://doi.org/10.2514/6.2003-4805
Publikováno v:
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
The quasi-3D CFD approach presented by Wang 1 for 3-D SRM ignition transient flow has been applied to perform predictions for static firings. The results of two interesting cases are presented in this paper. For the first case, Case-A, the motor has
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::75b6dfe4e4206076a303654f087084d1
https://doi.org/10.2514/6.2003-5115
https://doi.org/10.2514/6.2003-5115
Autor:
E. Stampfl, E. M. Landsbaum
Publikováno v:
Journal of Spacecraft and Rockets. 12:599-607
The erosion rate of aft closure insulation in a number of large solid propellant motors was empirically analyzed by correlating the average ablation rate with a number of variables that had previously been demonstrated to affect heat flux. The main c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::94659d47fbc8b3faac1e500b924c95a9
https://doi.org/10.2514/3.57024
https://doi.org/10.2514/3.57024
Publikováno v:
Journal of Spacecraft and Rockets. 17:400-406
The methods for the theoretical prediction of delivered specific impulse are relatively well known. They involve computing the losses due to two-phase flow, divergence, boundary layer, kinetics, nozzle submergence, and combustion inefficiency. The la
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::38cf066fdb8aa96df69a126e2a6fcbba
https://doi.org/10.2514/3.57758
https://doi.org/10.2514/3.57758
Publikováno v:
Industrial & Engineering Chemistry. 47:101-103
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::08869e2f16eff4b014459d871ded1687
https://doi.org/10.1021/ie50541a036
https://doi.org/10.1021/ie50541a036
Publikováno v:
AIChE Journal. 1:302-304
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::70b801291bef2c51862386b5a9618f95
https://doi.org/10.1002/aic.690010305
https://doi.org/10.1002/aic.690010305
Autor:
S. D. Heister, E. M. Landsbaum
Publikováno v:
21st Joint Propulsion Conference.
Ballistic anomalies, defined as pressure deviations from the normally expected trace, have occurred frequently during solid rocket motor firings. This paper describes techniques for determining the probable cause of such anomalies. Mass and energy ba
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d56d3b1071e939899465c7928d85cbf6
https://doi.org/10.2514/6.1985-1303
https://doi.org/10.2514/6.1985-1303