Mission Description

• Launch from Earth in 2002 (otherwise free)
• Flyby Venus in 2002,2004
• Flyby Jupiter 2453775.5 (Feb 9, 2006)
• Launch Vehicle: Delta 7925-9.5; 10% launch vehicle contingency
• Propulsion Model: Electric Engine G (1 or 2 Engines)
• Power Model: apsa1 solar array, P0 = 6.75 kW, Psc = 0
• Objective function: final mass
• Originally modeled using SEPTOP

Additional Mission Options

A. Same as Reference Case 8 except go to Pluto with arrival date of 2456896.5 (Aug 27, 2017)

Input/Output files

Copernicus20060310.zip (download)

MALTO4_3_2.zip (download)

SEPTOP11_136.zip (download)

All Reference Case 8: Earth - Venus/Venus/Jupiter Flybys - Pluto Flyby files (download zip)