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Dr. John Olson - NASA

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Transportation and Destination Architectures<br />

for Flexible Path (Initial Version)<br />

TRANSPORTATION ARCHITECTURE<br />

Multi-Purpose<br />

Crew Vehicle<br />

(MPCV)<br />

Space Launch<br />

System - HLLV<br />

In-Space<br />

Propulsion Stages<br />

Cryogenic<br />

Propulsion Stage<br />

(CPS)<br />

Solar Electric<br />

Propulsion (SEP)<br />

* MPCV Service Module derived Kick Stage utilized in<br />

some DRMs<br />

Elements based on Authorization Act and other<br />

conditions. Different constraint basis would result in<br />

different elements, but capabilities represented would<br />

be unchanged.<br />

DISTANCES AND<br />

ENVIRONMENTS<br />

LEO<br />

GEO/HEO<br />

Lunar<br />

NEA<br />

Mars<br />

DESTINATION<br />

ARCHITECTURE<br />

Crew EVA Suit<br />

(Block 1)<br />

Robotics & EVA<br />

Module (REM) or<br />

Space Exportation<br />

Vehicle (SEV)<br />

Lunar Lander<br />

International GPOD<br />

Surface Elements<br />

Crew EVA Suit<br />

(Block 2)<br />

Deep Space Habitat<br />

(DSH)<br />

Mars Lander &<br />

Additional Elements<br />

11

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