The vehicle(s) and associated systems will support U.S. ISS requirements for crew rescue, crew transport, and cargo.
1. The system, which may include multiple vehicles, shall provide rescue* capability for no fewer than four ISS crew as soon as practical but no later than 2010.
2. The system shall provide rescue capability that allows the safe return of deconditioned, ill or injured crewmembers with ongoing treatment until arrival at definitive medical care within 24 hours. Crew should not require suits in the vehicle, but the vehicle should support crew wearing suits if the situation warrants.
3. The system for rescue shall provide for rapid separation from the ISS under emergency conditions followed by return to Earth.
4. Safety requirements – system for crew rescue:
a. The availability (defined as “a full-up vehicle able to perform its mission”) for the escape mission shall be at least:
b. The risk of loss of crew shall be, with high confidence, lower than the Soyuz for the rescue mission.
Minimum Threshold: 95%.
5. The system shall provide transportation capability for no fewer than four crew to and from the ISS as soon as practical but no later than 2012.
6. Safety requirement – system for crew transport: The risk of loss of crew shall be, with high confidence, lower than the Space Shuttle for the transport mission.
7. The system shall be designed for minimum life cycle cost.
8. The system shall meet all applicable ISS requirements for visiting and attached vehicles.
9. Compared to the Space Shuttle, the system shall require less time to prepare and execute a mission and have increased launch probability.
10. Compared to the Space Shuttle, the system shall have increased on-orbit maneuverability.
1. The vehicle(s) shall initially launch on an ELV.
2. The system shall be operated through at least 2020. However, the system should be designed so that it could be operated for a longer time.
3. NASA envisions that the systems for crew rescue and crew transport could be different versions of the same vehicle design.
4. The system shall provide contingency capability for cargo delivery to or from the ISS to support a minimal level of science.
5. The system shall support a nominal ISS crew rotation period of 4-6 months.