Accession Number:

AD0607849

Title:

SATELLITE RENDEZVOUS TRAJECTORIES.

Personal Author(s):

Corporate Author:

NORTHROP SPACE LABS HAWTHORNE CALIF

Report Date:

1962-04-01

Abstract:

Two types of satellite rendezvous trajectories were discussed direct ascent from burnout and transfer from a parking orbit coplanar with the target orbit. Equations for the orbital elements and velocity requirements of the trajectories were presented, and numerical solutions were obtained for selected trajectories. Author

Descriptive Note:

Technical memo.

Supplementary Note:

Formerly released by Astro Systems and Research Labs., Norair Div., Northrop Corp., Hawthorne, Calif. as ASRL-TM-60-24, Oct. 60.

Pages:

0028

Descriptors:

Communities Of Interest:

Modernization Areas:

File Size:

0.00MB

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