Trajectory Design From GTO To Lunar Equatorial Orbit For The Dark Ages Radio Explorer (DARE) Spacecraft

Anthony L. Genova; Fan Yang Yang; Andres Dono Perez; Ken F. Galal; Nicolas T. Faber; Scott Mitchell; Brett Landin; Abhirup Datta; Jack O. Burns

arXiv · 1504.00410

Trajectory Design From GTO To Lunar Equatorial Orbit For The Dark Ages Radio Explorer (DARE) Spacecraft

Anthony L. Genova·Fan Yang Yang·Andres Dono Perez·Ken F. Galal·Nicolas T. Faber·Scott Mitchell·Brett Landin·Abhirup Datta·Jack O. Burns

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Abstract

The trajectory design for the Dark Ages Radio Explorer (DARE) mission con-cept involves launching the DARE spacecraft into a geosynchronous transfer orbit (GTO) as a secondary payload. From GTO, the spacecraft then transfers to a lunar orbit that is stable (i.e., no station-keeping maneuvers are required with minimum perilune altitude always above 40 km) and allows for more than 1,000 cumulative hours for science measurements in the radio-quiet region located on the lunar farside.

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Anthony L. Genova, Fan Yang Yang, Andres Dono Perez, Ken F. Galal, Nicolas T. Faber, Scott Mitchell, Brett Landin, Abhirup Datta, Jack O. Burns. 2015-04-01. Trajectory Design From GTO To Lunar Equatorial Orbit For The Dark Ages Radio Explorer (DARE) Spacecraft. https://arxiv.org/abs/1504.00410

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