Mission Description

• Earth.s orbit semi-major axis 149597870:691 km
  • Mars.orbit semi-major axis (1:5236623)(149597870:691) = 227936635:732 km
  • Initial mass 4536 kg
  • engine thrust 3:781 Newton
  • engine Isp 5693.0 sec
  • Originally modeled in Copernicus

  Additional Mission Options

  A. Another variant...

  • Propulsion System SEP
  • Launch Date 2003 (free)
  • Rendezvous Date 2004 (free)
  • Solar Array ASPA 1
  • Engine NSTAR Engine G (1 engine)
  • P0 11 kW
  • Duty Cycle 100%
  • Launch Vehicle Delta 7326-9.5
  • Initial Mass 650 kg (fixed)
  • Originally modeled in MALTO

  Input/Output files

  Copernicus20060313.zip (download)

  MALTO4_4.zip (download)

  All Reference Case 13:  Classic minimum time to Mars, circular/coplanar Files (download zip)