Labels:text | diagram | line | font | plot OCR: Trajectory Characteristics Assumptions 7- Y-infinity at Mars arrival 2005 Launch Launch from SSF orbit 6. 250 km x 1 sol orbit at Mars 37t pay load 5. delivered to Mars surface (km/sec) 4 Y TMI Aerobrake to 500 km circular phasing orbit, 3. then deorbit 2. 100 150 200 250 Earth to Mars Flight-time (days)
