2 edition of Water-propellant resistojets for man-tended platforms found in the catalog.
Water-propellant resistojets for man-tended platforms
by National Aeronautics and Space Administration, For sale by the National Technical Information Service in [Washington, DC], [Springfield, Va
Written in English
|Other titles||Water propellant resistojets for man-tended platforms.|
|Statement||Allen J. Louviere ... [et al.].|
|Series||NASA technical memorandum -- 100110., IAF-87-259, IAF (Series) -- 87-259.|
|Contributions||Louviere, Allen J., United States. National Aeronautics and Space Administration.|
|The Physical Object|
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Water has been selected as the propellant for this man-tended platform. Water meets all of the requlrements mentloned above and with suitable planning can be made avallable by utllizlng water from environmental control systems, either on the Space Shuttle Orbiter File Size: 3MB.
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The selection of a propulsion system for a man-tended platform has been influenced by the planned use of resistojets for drag make-up on the manned space station. For that application a resistojet has been designed that is capable of operation with a wide variety of propellants, including water.
Louviere, Allen J. et al "Water-Propellant Resistojets for Man- Tended Platforms", NASA Technical MemorandumPhoto-thermal Engines [ edit ] This group uses direct electromagnetic radiation (photons) from natural or artificial sources to heat the propellant. late 's water resistojets were baselined to provide all propulsion for the Industrial Space Facility (ISF), a man-tended commercial platform originally scheduled for launch in the early 's.2 Water resistojets were also considered for atmospheric drag cancellation on Space Station Freedom (SSF).
Water resistojets have someFile Size: 7MB. This paper discusses the reasons for selection of water as the propellant and the performance of resistojets using water, and describes the man-tended platform and its mission requirements.
Water resistojets have also been baselined for orbit maintenance duty on the man-tended Indus- trial Space Facility scheduled for launch in the early 's.2 The use of water as a reslstojet propellant for manned or man-tended platforms has a number of attractive features.
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The remarkable features of the system are the usage of water propellant and unification of the two types of thrusters by the single propellant.
Water has been regarded as an attractive propellant in the view points of safety, availability, handling ability, low Cited by: 2. The theme of this book is an exposition of what we know about the physicsunderlying the onset of instability in liquid sheets and jets.
Wave motionand breakup phenomena subsequent to the onset of instability are alsocarefully by: CubeSats provide a cost effective means to perform scientific and technological studies in space.
Due to their affordability, CubeSat technologies have been diversely studied and developed by educational institutions, companies and space organizations all over the world. The CubeSat technology that is surveyed in this paper is the propulsion system.
A propulsion system is the Cited by: C. Bader, Potential propellant storage and feed systems for space station resistojet propulsion options. NASA CR (). Gruber, Resistojet control and power for high frequency, AC buses.
NASA TM AIAA Paper (). Louviere et al., Water propellant resistojets for man-tended platforms. NASA TM Cited by: 5.
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et al "Water-Propellant Resistojets for Man- Tended Platforms", NASA Technical Memorandum37 Solar-Thermal Alternate Names: Type: Description: Sunlight is concentrated by a reflector or lens, then heats an absorber.
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Duchêne, John H. Ledeboer, T. O'b. Hubbard. Several cold gas propulsion systems have been developed for the CubeSat platform, and they are the most mature type of propulsion system for CubeSats.
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