Optical ascent into orbit - a new look at an old problem.

Optimum thrust programming of ascent trajectory for orbiting space vehicle, using parameter variation method

Document ID

19650028160

Acquisition Source

Legacy CDMS

Document Type

Conference Paper

Authors

Date Acquired

August 2, 2013

Publication Date

September 1, 1964

Subject Category

Accession Number

65A10864

Distribution Limits

Public

Other

Keywords

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