Thrust efficiencies of electromagnetic engines.

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Ionized plasma electromagnetic accelerators, noting thrust efficiency variation due to difference between supplied and expelled mass flow rate

Document ID

19680038893

Acquisition Source

Legacy CDMS

Document Type

Reprint (Version printed in journal)

Authors

Date Acquired

August 4, 2013

Publication Date

March 1, 1968

Publication Information

Publisher: AIAA JOURNAL, VOL. 6, P. 558-560.

Subject Category

Accession Number

68A19865

Funding Number(s)

Distribution Limits

Public

Other

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