Application of an iterative guidance mode to a lunar landing <anwendung eines iterativen lenkverfahren auf eine mondlandung<.

Application of an iterative guidance mode to a lunar landing

Iterative guidance mode applied to lunar landing for optimization of trajectories for minimum propellant consumption

Document ID

19640032645

Acquisition Source

Legacy CDMS

Document Type

Reprint (Version printed in journal)

Authors

Date Acquired

August 2, 2013

Publication Date

June 1, 1964

Subject Category

Accession Number

64A18538

Distribution Limits

Public

Other

Keywords

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