Mission Description

• Launch from Earth in 2002 (otherwise free)
• Flyby Jupiter on Julian date 2454250.5 (May 30,2007) -- fixed
• Launch Vehicle: Delta 7925-9.5; 10% launch vehicle contingency
• Propulsion Model: Electric Engine J (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 9 except now v-infinity is 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 9: Earth - [>1 rev around the Sun] - Jupiter Flyby Files (download zip)