Design and Testing of a Chemical Injection System for Reentry Plasma Alleviation PDF Download
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Author: John F. Lennon Publisher: ISBN: Category : Fluorohydrocarbons Languages : en Pages : 52
Book Description
The effect of injecting an electrophilic liquid into the ionized flow field surrounding a reentry vehicle was observed during the flight of a trailblazer 2 on 28 July 1972. The report describes the rationale used to initially screen candidate additives and the experimental evaluation that finally resulted in the selection of Freon 114B2 for operational use. Injection system design and preliminary testing are discussed, and the predicted and actual performance during flight are compared. Data from on-board antennas and electrostatic probes confirmed that the additive reduced the electron density and improved transmission. A number of factors characterizing the injection are presented as a basis for analyzing the flow-additive interaction. (Author).
Author: John F. Lennon Publisher: ISBN: Category : Fluorohydrocarbons Languages : en Pages : 52
Book Description
The effect of injecting an electrophilic liquid into the ionized flow field surrounding a reentry vehicle was observed during the flight of a trailblazer 2 on 28 July 1972. The report describes the rationale used to initially screen candidate additives and the experimental evaluation that finally resulted in the selection of Freon 114B2 for operational use. Injection system design and preliminary testing are discussed, and the predicted and actual performance during flight are compared. Data from on-board antennas and electrostatic probes confirmed that the additive reduced the electron density and improved transmission. A number of factors characterizing the injection are presented as a basis for analyzing the flow-additive interaction. (Author).
Author: Publisher: ISBN: Category : Languages : en Pages : 0
Book Description
The effect of injecting an electrophilic liquid into the ionized flow field surrounding a reentry vehicle was observed during the flight of a trailblazer 2 on 28 July 1972. The report describes the rationale used to initially screen candidate additives and the experimental evaluation that finally resulted in the selection of Freon 114B2 for operational use. Injection system design and preliminary testing are discussed, and the predicted and actual performance during flight are compared. Data from on-board antennas and electrostatic probes confirmed that the additive reduced the electron density and improved transmission. A number of factors characterizing the injection are presented as a basis for analyzing the flow-additive interaction. (Author).
Author: Publisher: ISBN: Category : Aeronautics Languages : en Pages : 456
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author: Humberto Luis Caldelas (II) Publisher: ISBN: Category : Languages : en Pages : 169
Book Description
This thesis contains information authorized for DISTRIBUTION A: Approved for Public release via AEDC Information Release Authority IRA-5647, PA AEDC2021-084. This thesis contains patent information protected by the MIT Technology Licensing Office under MIT Case Number 23238. Information has been excluded/redacted from this thesis in order to adhere to the aforementioned distribution statement and patent protection requirements.
Author: John F. Lennon
Author: John F. Lennon
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Author: Air Force Cambridge Research Laboratories (U.S.)
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Author: Humberto Luis Caldelas (II)
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Author: Scripps Institution of Oceanography. Library