Transient reactive exhaust flow from a ring-symmetric HF/DF space laser

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Last edited by MARC Bot
September 8, 2021 | History

Transient reactive exhaust flow from a ring-symmetric HF/DF space laser

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Transient diffuser flow in an HF/DF laser is analyzed via a simplified model. A radial laser configuration is assumed where the diffuser is idealized as a ring-symmetric channel of uniform width. The outward radial flow following an abrupt start-up of diffuser inflow is computed numerically using a GRP-type code for integrating the Euler equations, which include an ongoing reaction of hydrogen recombination. A new kinetic scattering effect is suggested, resulting from the recoil of an HF or DF molecule assisting as third body in the hydrogen recombination reaction. The main conclusion is that transient diffuser plume flow effects do not drastically aggravate the potential for contaminating backflow (HF + DF) caused by either thermal or kinetic backscattering. Keywords: Laser exhaust; Spacecraft contamination; Chemical laser; Exhaust plume, Hydrogen recombination; Transient flow.

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Cover of: Transient reactive exhaust flow from a ring-symmetric HF/DF space laser
Transient reactive exhaust flow from a ring-symmetric HF/DF space laser
1987, Naval Postgraduate School, Available from National Technical Information Service
in English

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Book Details


Edition Notes

Title from cover.

"NPS-72-87-002CR."

"March 1987."

AD A179 208.

Includes bibliographical references (p. 18-19).

Published in
Monterey, Calif, Springfield, Va
Other Titles
NPS-72-87-002CR.

The Physical Object

Pagination
vi, 45 p.
Number of pages
45

ID Numbers

Open Library
OL33220440M
Internet Archive
transientreactiv00falc

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