Explicit guidance equations for multistage boost trajectories

Explicit equations for steering Atlas-Centaur multistage launch vehicle to lunar trajectory

Document ID

19660006073

Document Type

Other - NASA Technical Note (TN)

Authors

Teren, F. (NASA Lewis Research Center Cleveland, OH, United States)

Date Acquired

September 2, 2013

Publication Date

January 1, 1966

Subject Category

Report/Patent Number

Distribution Limits

Public

Work of the US Gov. Public Use Permitted.

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