Minimum propellant consumption round-trip trajectories to Mars for constant-thrust, constant-specific-impulse vehicles with optimum coasting periods

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Minimum propellant consumption trajectories to Mars for constant-thrust, constant-specific impulse vehicles with optimum coasting periods

Document ID

19660006201

Acquisition Source

Legacy CDMS

Document Type

Other - NASA Technical Note (TN)

Authors

Date Acquired

September 2, 2013

Publication Date

January 1, 1966

Subject Category

Report/Patent Number

Accession Number

66N15490

Distribution Limits

Public

Work of the US Gov. Public Use Permitted.

Keywords

Name

Type

STI

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