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Demonstrated Heavy Lift Capability

Fewer Launches + Fewer Payloads + Fewer In-space Assemblies = Higher Mission Reliability

Single Launch: 320,000 Pounds to LEO

• Replace Space Shuttle orbiter with in-line configuration that can carry significantly more payload
• Demonstrated reliability of propulsion system heritage

Highest Mission Reliability

• A single launch of 320,000 lb to LEO is able to do the job of seven launches of 45,000 to 50,000 lb
• Eliminates costly/complex in-space docking, on-orbit assembly, and checkout
• Simplifies payload/mission architecture, design, and logistics
• Lowest cost/risk