Zobrazeno 1 - 10
of 17
pro vyhledávání: '"E. E. Zhabotinskii"'
Publikováno v:
Atomic Energy. 75:762-765
Space technology for manufacturing on an industrial scale of certain materials, and medicines of significantly higher quality. At present, space manufacturing of semiconductor materials for the electronic industry seems the most promising. Even in th
Autor:
Georgy M. Gryaznov, A. Ya. Galkin, Anatoly M. Nikonov, Pavel V. Andreev, Victor I. Serbin, G. A. Zaritskii, E. E. Zhabotinskii
Publikováno v:
Atomic Energy. 75:757-761
Power-generation and propulsion complexes for spacecraft, universal space platforms (US) which combine a power unit and high- and low-thrust propulsion unions, make it possible to efficiently solve problems involved in creating satellite communicatio
Publikováno v:
Atomic Energy. 75:766-769
The parameters of a thermoelectric reactor are determined by the radial dimensions of the EGC, in particular the external diameter d{sub EGC}, the diameter d{sub e} of the emitter, and the diameter d{sub c} of the channel fuel core. In this paper we
Publikováno v:
Atomic Energy. 73:857-860
Publikováno v:
Atomic Energy. 72:224-229
Publikováno v:
Soviet Atomic Energy. 71:1041-1044
Successful ground and flight tests of the “Topaz” NPP have made it possible to conclude that thermal-emission NPPs of this type should have a control algorithm that for the thermal state of the NPP and, primarily, the cesium-vapor-supply system.
Publikováno v:
Soviet Atomic Energy. 71:882-887
Publikováno v:
Soviet Atomic Energy. 71:877-881
Flight tests of two production models of the NPU “Topaz” confirmed the correspondence of the thermal state of the NPU assembly to the formulated limits throughout prestart preparation, launch, and orbital flight. Thus was shown the well-establish
Autor:
G. M. Gryaznov, P. V. Andreev, E. E. Zhabotinskii, G. A. Zaritskii, V. I. Serbin, A. M. Nikonov
Publikováno v:
Soviet Atomic Energy. 70:271-275
Publikováno v:
Soviet Atomic Energy. 70:275-279
The use of a thermionic NPS with a thermal reactor in space technology to supply power to the RMPS offers broad possibilities for interorbital delivery of payloads while using comparatively cheap launch rockets to place spacecraft in a fixed orbit. T