The PEGASUS Drive: A nuclear electric propulsion system for the space exploration initiative

Conference · Mon Oct 01 00:00:00 EDT 1990

OSTI ID:6399282

Coomes, E P; Dagle, J E

The advantages of using electric propulsion for propulsion are well-known in the aerospace community. The high specific impulse, lower propellant requirements, and lower system mass make it a very attractive propulsion option for the Space Exploration Initiative (SEI), especially for the transport of cargo. One such propulsion system is the PEGASUS Drive (Coomes et al. 1987). In its original configuration, the PEGASUS Drive consisted of a 10-MWe power source coupled to a 6-MW magnetoplasmadynamic (MPD) thruster system. The PEGASUS Drive propelled a manned vehicle to Mars and back in 601 days. By removing the crew and their associated support systems from the spacecraft and by incorporating technology advances in reactor design and heat rejection systems, a second generation PEGASUS Drive can be developed with an alpha less than two. Utilizing this propulsion system, a 400-MT cargo vehicle, assembled and loaded in low Earth orbit (LEO), could deliver 262 MT of supplies and hardware to Mars 282 days after escaping Earth orbit. Upon arrival at Mars the transport vehicle would place its cargo in the desired parking orbit around Mars and then proceed to synchronous orbit above the desired landing sight. Using a laser transmitter, PEGASUS would provide 2-MWe on the surface to operate automated systems deployed earlier and then provide surface power to support crew activities after their arrival. The additional supplies and hardware, coupled with the availability of megawatt levels of electric power on the Mars surface, would greatly enhance and even expand the mission options being considered under SEI. 9 refs., 1 fig., 1 tab.

• Research Organization: Pacific Northwest Lab., Richland, WA (USA)
• Sponsoring Organization: DOE/NE
• DOE Contract Number: AC06-76RL01830
• OSTI ID: 6399282
• Report Number(s): PNL-SA-18827; CONF-910116-9; ON: DE91004734
• Resource Relation: Conference: 8. symposium on space nuclear power systems, Albuquerque, NM (USA), 6-10 Jan 1991
• Country of Publication: United States
• Language: English

Related Subjects

21 SPECIFIC NUCLEAR REACTORS AND ASSOCIATED PLANTS
MARS SPACE PROBES
SPACE POWER REACTORS
DESIGN
SPACE VEHICLES
SPACE PROPULSION REACTORS
HEAT TRANSFER
MAGNETOGASDYNAMICS
MISSION ANALYSIS
REACTOR CONTROL SYSTEMS
SHIELDING
SPACE TRANSPORT
SPACE VEHICLE COMPONENTS
THRUSTERS
CONTROL SYSTEMS
ENERGY TRANSFER
FLUID MECHANICS
MECHANICS
MOBILE REACTORS
POWER REACTORS
PROPULSION REACTORS
REACTORS
TRANSPORT
VEHICLES
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