Zobrazeno 1 - 5
of 5
pro vyhledávání: '"T. A. Coultas"'
Publikováno v:
Journal of Spacecraft and Rockets. 1:643-648
With the advent of solid rocket engines utilizing high-energy aluminized propellants, the need for a noneroding nozzle-throat insert material has become acute. The wall temperatures attained at the throat are above even the maximum practical operatin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d679f1249fa2aedd5ab3125bc586cd28
https://doi.org/10.2514/3.27715
https://doi.org/10.2514/3.27715
Autor:
T. A. Coultas
Publikováno v:
Journal of Chemical & Engineering Data. 8:527-530
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8534e1b62783661aea3b2a9bef8dfed6
https://doi.org/10.1021/je60019a015
https://doi.org/10.1021/je60019a015
Autor:
T. A. Coultas, A. L. Huebner
Publikováno v:
2nd Propulsion Joint Specialist Conference.
A measure of the effect of solid propellant combustion upon pressure perturbations arising in a rocket chamber is provided by the response function of the burning surface. Conventional methods of measuring this quantity are based upon a number of ass
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::24849ffb359c0679163e9365d477751a
https://doi.org/10.2514/6.1966-601
https://doi.org/10.2514/6.1966-601
Autor:
H. L. Burge, T. A. Coultas
Publikováno v:
SAE Technical Paper Series.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e0604dc4bae7997146455c4379014555
https://doi.org/10.4271/600388
https://doi.org/10.4271/600388