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Results for “LuNi”

Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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56 records · Page 4

All sources NASA NTRS DOE OSTI

NASA NTRS1993

Using Anomalous Along-Track Forces for Topex/Poseidon Ground Track Control

The TOPES/POSEIDON satellite is maintained in a nearly circular, frozen orbit at an altitude of =1336 km. and an inclination of i = 66.4, which provides an exact repeat ground track every 127 revolutions and overflies two altimetry verifications sites.

outgassing↗

NASA NTRS2015

MLTAN: Theory and Practice

No abstract available

Luni-solar perturbation↗