CEAS Space Journal

, Volume 3, Issue 1–2, pp 49–59 | Cite as

Weak stability boundary transfer to the Moon from GTO as a piggyback payload on Ariane 5

  • Dominik Quantius
  • Jörn Spurmann
  • Erwin Dekens
  • Hartmut Päsler
Original Paper

Abstract

In cooperation with the German non-profit amateur satellite organisation (AMSAT-DL), the German Aerospace Center developed the idea of using AMSAT’s Earth satellite P3-D as a baseline for a Moon mission. For cost-effectiveness, P3-D was launched as an auxiliary payload on Ariane 5 into a geosynchronous transfer orbit (GTO) and used its on-board propulsion system to achieve a Molniya orbit. The present study describes how a similar satellite can reach a 100 × 100 km lunar orbit with the same launch strategy. A delta-v saving transfer scenario using the weak stability boundary transfer was found to be feasible taking a P3-D-like satellite bus into account. It contains phasing orbits as a solution for non-dedicated launch dates and deals with the constraints of Ariane’s GTO. This approach opens up the opportunity to accomplish a low-cost mission to the Moon with public and scientific value.

Keywords

DLR-AMSAT P5 Moon WSB Auxiliary payload Open source Lunar orbit Low-cost satellite Lunar television 

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Copyright information

© CEAS 2012

Authors and Affiliations

  • Dominik Quantius
    • 1
  • Jörn Spurmann
    • 3
  • Erwin Dekens
    • 1
  • Hartmut Päsler
    • 2
  1. 1.DLR German Aerospace CenterBremenGermany
  2. 2.AMSAT-DLMarburgGermany
  3. 3.DLR German Aerospace CenterOberpfaffenhofenGermany

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