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Figure 4 from NUCLEAR THERMAL ROCKET/VEHICLE CHARACTERISTICS AND SENSITIVITY TRADES FOR NASA's MARS DESIGN REFERENCE ARCHITECTURE (DRA) 5.0 STUDY

Figure 4 from NUCLEAR THERMAL ROCKET/VEHICLE CHARACTERISTICS AND  SENSITIVITY TRADES FOR NASA's MARS DESIGN REFERENCE ARCHITECTURE (DRA) 5.0  STUDY

Figure 4 from NUCLEAR THERMAL ROCKET/VEHICLE CHARACTERISTICS AND SENSITIVITY TRADES FOR NASA's MARS DESIGN REFERENCE ARCHITECTURE (DRA) 5.0 STUDY

PDF] Modular Growth NTR Space Transportation System for Future NASA Human Lunar, NEA and Mars Exploration Missions

Realistic Designs A-G - Atomic Rockets

PDF] HERRO Mission to Mars Using Telerobotic Surface Exploration from Orbit

PDF] Modular Growth NTR Space Transportation System for Future NASA Human Lunar, NEA and Mars Exploration Missions

LEU NTP Part Three: Spacecraft Overview – Beyond NERVA

PDF] Modular Growth NTR Space Transportation System for Future NASA Human Lunar, NEA and Mars Exploration Missions

PDF) Nuclear Thermal Propulsion for Jupiter and Saturn Rendezvous Missions

Figure 4 from NUCLEAR THERMAL ROCKET/VEHICLE CHARACTERISTICS AND SENSITIVITY TRADES FOR NASA's MARS DESIGN REFERENCE ARCHITECTURE (DRA) 5.0 STUDY

PDF) Human exploration of Mars, Design Reference Architecture 5.0

PDF) Nuclear Thermal Rocket/vehicle design options for future NASA missions to the Moon and Mars

Full article: Preliminary Conceptual Design of Nuclear Thermal Rocket Reactor Cores Using Ceramic Fuels with Beryllium or Composite Neutron Moderators

NTP – Beyond NERVA

Realistic Designs A-G - Atomic Rockets