Mission Description

• Launch from Earth in 2004, otherwise free
• Flyby Venus on Julian date 2453970.5 (Aug 23, 2006) -- fixed
• Flyby Jupiter on Julian date 2454712.5 (Sep 3, 2008) -- fixed
• Initial mass: free
• Launch V∞ magnitude: free
• Launch V∞ direction is free
• Launch Vehicle = Delta 7925-9.5
• Propulsion Model: Electric Engine G (1 or 2 Engines)
• Power Model: apsa1 solar array, P0 = 7.0 kW, Psc = 0.1kW
• Objective function: final mass
• Originally modeled using SEPTOP

Additional Mission Options

A. Same as Reference Case 6 except now the Venus flyby date is free.
B. Same as Reference Case 6 except now the arrival date is free.
C. Same as Reference Case 6 except change the ref power to 5.0 kW
D. Same as Reference Case 6 except now the Venus Flyby and Jupiter Arrival dates are free.

Input/Output files

Copernicus20060310.zip (download)

MALTO4_3_2.zip (download)

Mystic9_0_0.zip (download)

SEPTOP11_136.zip (download)

All Reference Case 6: Earth - Venus Flyby - Jupiter Flyby files (download zip)