Mission Description

• Launch from Earth in 2002, otherwise free
• Flyby Jupiter on Julian date 2453687.5, Nov 13, 2005 (fixed)
• Launch V∞ magnitude:   free
• Launch V∞ direction is free
• Launch Vehicle:  Delta 7925-9.5
• 10% Launch Vehicle Contingency
• Propulsion Model:  Electric Engine G (1,2, or 3 Engines)
• Power Model: apsa1 solar array, P0 = 11.0 kW, Psc = 0
• Objective function:  final mass
• Originally modeled using SEPTOP

Additional Mission Options

A. Same as Reference Case 5, except that the v-inf is now fixed at 4.4 km/sec
B. Same as Reference Case 5, except that the Jupiter flyby date is free.
C. Same as Reference Case 5, except that the reference power is altered to 7.0 kW.
D. Same as Reference Case 5 except that the reference power and arrival date are both free.

Input/Output files

CHEBYTOPv6.zip (download)

Copernicus20060310.zip (download)

MALTO4_3_2.zip (download)

Mystic9_0_0.zip (download)

SEPTOP11_136.zip (download)

All Reference Case 5:  Earth - Jupiter Flyby Files (download zip)