Orbital transfer vehicle oxygen turbopump technology
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Orbital transfer vehicle oxygen turbopump technology test series F&G, task b.8 final report by

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Published by Gencorp Aeroject, Propulsion Division, National Aeronautics and Space Administration, National Technical Information Service, distributor in [Sacramento, Calif.], [Washington, DC, Springfield, Va .
Written in English


  • Fluid-film bearings.

Book details:

Edition Notes

Statementprepared by Robert L. Urke.
SeriesNASA contractor report -- NASA CR-191036-
ContributionsUnited States. National Aeronautics and Space Administration.
The Physical Object
ID Numbers
Open LibraryOL17680430M

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Get this from a library! Orbital transfer vehicle oxygen turbopump technology. Volume I, Design, fabrication, and hydrostatic bearing testing: final report. [P S Buckmann; United States. National Aeronautics and Space Administration.; Lewis Research Center.;]. testing of an advanced oxygen turbopump required for the Space Based Orbit Transfer Vehicle Propulsion System employing the Aerojet dual propellant expander cycle. The experimental results reported herein are applicable to a wide range of components and applications in which high pressure oxygen flowsFile Size: 7MB. of liquid oxygen per second. The Block I engine also incorporated a two-duct powerhead, which improved the distribution of the fuel flow and reduced the pressure and temperature in the engine, and a single-coil heat exchanger, which eliminated welds and increased reliability. In addition, the new oxygen turbopump included newFile Size: KB. Full text of "Orbital transfer vehicle concept definition and system analysis 2: OTV concept definition and evaluation. Book 3: Subsystem trade studies" See other formats.

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  So IVF combined with cryocooler technology should make reusable LOX/LH2 vehicles for lunar and Mars landings and for interplanetary orbital transfer vehicles and propellant depots a reality by the late s. An orbital transfer vehicle, or “space tug,” is one instance of a broad class of vehicles that can perform a variety of on-orbit servicing functions. The simplest function of such a vehicle would be to observe space assets, hereafter referred to as targets, in situ. The targets may be cooperative (designed for servicing),File Size: 1MB. Animation & Cartoons Arts & Music Computers & Technology Cultural & Academic Films Ephemeral Films Movies News & Public Affairs. Understanding 9/ Spirituality & Religion Sports Videos Television Videogame Videos Vlogs Youth Media. Full text of "Two designs for an orbital transfer vehicle". Electric propulsion for orbital transfer Power lost due to irradiation (kW) Transfer time (days) Power required (kW) 14 To minimise the cost and size of the solar cell array therefore and to minimise the cost of the power lost during transfer as long a transfer time as possible is : R.C. Godwin, T. Rees.