Zobrazeno 1 - 6
of 6
pro vyhledávání: '"S. C. Debrock"'
Autor:
R. K. Grove, S. C. Debrock
Publikováno v:
Journal of Spacecraft and Rockets. 12:261-270
Early Agena orbital vehicles have utilized separate propellant tanks for the primary orbit injection and secondary orbit adjust propulsion subsystems. After orbit injection, much of the primary propulsion system propellants remained but were unavaila
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bc3ae51cf1b0ed07decb3a82a818dda6
https://doi.org/10.2514/3.56972
https://doi.org/10.2514/3.56972
Autor:
C. J. Rudey, S. C. Debrock
Publikováno v:
Journal of Spacecraft and Rockets. 11:769-777
T Agena is a space-proven, multipurpose space vehicle which is capable of ascent, precision orbit injection, and spacecraft missions from low Earth orbit to interplanetary transfers. The Agena upper stage has been boosted by Thorad, Atlas, and Titan
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::51c3602fd46d023411b0eba29b2e35b1
https://doi.org/10.2514/3.62175
https://doi.org/10.2514/3.62175
Autor:
S. C. Debrock, M. W. Dowdy
Publikováno v:
Journal of Spacecraft and Rockets. 10:549-558
Discussion of the propellant management system requirements derived for the Viking 75 mission, and review of a series of surface tension propellant management system design concepts. The chosen concept is identified and its mission operation describe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::db5f38e9deeb0f63e8a00a29a3ccc54b
https://doi.org/10.2514/3.61925
https://doi.org/10.2514/3.61925
Autor:
M. A. Saad, S. C. Debrock
Publikováno v:
Journal of Spacecraft and Rockets. 3:1782-1788
plasticity of metals," Fundamentals of Deformation Processing (Syracuse University Press, Syracuse, N. Y., 1964), pp. 259298; also ASM Transactions (1962), Vol. 55, pp. 264-267. 4 Hatch, A. J., "Texture strengthening of titanium alloys," Trans. Am. I
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e6566ce9e33c95781b93ba6408609cd2
https://doi.org/10.2514/3.28748
https://doi.org/10.2514/3.28748
Autor:
S. C. Debrock, M. W. Dowdy
Publikováno v:
8th Joint Propulsion Specialist Conference.
Discussion of the propellant management system requirements derived for the Viking 75 mission, and review of a series of surface tension propellant management system design concepts. The chosen concept is identified and its mission operation describe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ce803322fe78e3f3e32c93d0b3fb5c4c
https://doi.org/10.2514/6.1972-1042
https://doi.org/10.2514/6.1972-1042
Autor:
S. C. Debrock
Publikováno v:
5th Propulsion Joint Specialist.
An Agena propulsion system performance model predicts the engine propellant flowrate and vehicle mass status; computes the over-all propellant mixture ratio required for propellant tank loading calculations; predicts the engine thrust time history ap
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::fd9d0c7564da621ec271cfeed54b31a5
https://doi.org/10.2514/6.1969-453
https://doi.org/10.2514/6.1969-453