Mars mission performance enhancement with hybrid nuclear propulsion
- Pacific Northwest Lab., Richland, WA (United States)
- USDOE Richland Operations Office, WA (United States)
Nuclear electric propulsion (NEP), compared with chemical and nuclear thermal propulsion (NTP), can effectively deliver the same mass to Mars using much less propellant, consequently requiring less mass delivered to Earth orbit. The lower thrust of NEP requires a spiral trajectory near planetary bodies, which significantly increases the travel time. Although the total travel time is long, the portion of the flight time spent during interplanetary transfer is shorter, because the vehicle is thrusting for much longer periods of time. This has led to the supposition that NEP, although very attractive for cargo missions, is not suitable for piloted missions to Mars. However, with the application of a hybrid application of a hybrid approach to propulsion, the benefits of NEP can be utilized while drastically reducing the overall travel time required. Development of a dual-mode system, which utilizes high-thrust NTP to propel the spacecraft from the planetary gravitational influence and low-thrust NEP to accelerate in interplanetary space, eliminates the spiral trajectory and results in a much faster transit time than could be obtained by either NEP or NTP alone. This results in a mission profile with a lower initial mass in low Earth orbit. In addition, the propulsion system would have the capability to provide electrical power for mission applications.
- Research Organization:
- Pacific Northwest National Laboratory (PNNL), Richland, WA (United States)
- Sponsoring Organization:
- USDOE, Washington, DC (United States)
- DOE Contract Number:
- AC06-76RL01830
- OSTI ID:
- 10117961
- Report Number(s):
- PNL-SA--20132; CONF-920104--29; ON: DE92006729
- Country of Publication:
- United States
- Language:
- English
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Advanced hybrid nuclear propulsion Mars mission performance enhancement
FAST INTERPLANETARY MISSIONS WITH LOW-THRUST PROPULSION SYSTEMS
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210500
210600
HEAT TRANSFER
LIQUID METAL COOLED REACTORS
MARS SPACE PROBES
MECHANICAL PROPERTIES
MISSION ANALYSIS
NESDPS Office of Nuclear Energy Space and Defense Power Systems
PERFORMANCE
PHYSICAL PROPERTIES
POWER REACTORS
BREEDING
POWER REACTORS, MOBILE, PROPULSION, PACKAGE, AND TRANSPORTABLE
PROPELLANTS
PROPULSION
PROPULSION SYSTEMS
RANKINE CYCLE POWER SYSTEMS
ROCKETS
SPACE FLIGHT
SPACE PROPULSION REACTORS
SPACE VEHICLES