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
|Statement||prepared by Robert L. Urke.|
|Series||NASA contractor report -- NASA CR-191036-|
|Contributions||United States. National Aeronautics and Space Administration.|
|The Physical Object|
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.
out of 5 stars Transfer pump. Reviewed in the United States on J Verified Purchase. Now this is a kool tool every home owner should have. But the hose needs to be longer. Read more. 3 people found this helpful. Helpful. Comment Report abuse. wine o. out of 5 stars must have/5(43). Liquid Rocket Engine Turbopump Inducers Paperback – Ap by National Aeronautics and Space Administration (Author) See all 3 formats and editions Hide other formats and editions. Price New from Used from Paperback "Please retry" $ $ Author: National Aeronautics and Space Administration. Vulcain is a family of European first stage rocket engines for Ariane 5 and the future Ariane development began in and the first flight was completed in The updated version of the engine, Vulcain 2, was first successfully flown in Both members of the family use liquid oxygen/liquid hydrogen cryogenic new version under development for Ariane 6 will be Country of origin: France. The SpaceX Raptor is a full-flow, staged-combustion, methane-fueled rocket engine manufactured by engine is powered by cryogenic liquid methane and liquid oxygen (LOX), rather than the RP-1 kerosene and LOX used in SpaceX's prior Merlin and Kestrel rocket engines. The earliest concepts for Raptor considered liquid hydrogen (LH 2) as fuel rather Application: Multistage propulsion.
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.