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Finite-thrust escape from and capture into circular and elliptic orbitsFinite-thrust escape and capture trajectories leading from circular or elliptic orbits to hyperbolic excess velocity vector located at gravitational sphere of influence
Document ID
19660027029
Document Type
Other - NASA Technical Note (TN)
Authors
Willis, E. A., Jr. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1966
Subject Category
SPACE SCIENCES
Report/Patent Number
NASA-TN-D-3606
Funding Number(s)
CONTRACT_GRANT: 121-30-02-01-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ESCAPE VELOCITY
HYPERBOLIC ORBIT
TRAJECTORY ANALYSIS

Available Downloads

NameType 19660027029.pdf STI