Mission Description

• Propulsion System SEP
• Launch Date 2011 (free)
• Rendezvous Date 2018 (free)
• Earth Return Date 2021 (free)
• Tempel 1 Stay Time 50 days (fixed)
• Mass Drop 0  (fixed)
• Solar Array ASPA 1
• Engine NSTAR Engine G (1 engine)
• P0 11 kW
• Duty Cycle 100%
• Launch Vehicle Delta 7326-9.5
• Originally modeled using MALTO

Input/Output files

Copernicus20060310.zip (download)

MALTO4_3_2.zip (download)

Mystic9_0_0.zip (download)

All Reference Case 11:  Tempel 1 Rendezvous - Earth Flyby Files (download zip)