SciTech Connect

Title: THE MARS HOPPER: AN IMPULSE DRIVEN, LONG RANGE, LONG-LIVED MOBILE PLATFORM UTILIZING IN-SITU MARTIAN RESOURCES

THE MARS HOPPER: AN IMPULSE DRIVEN, LONG RANGE, LONG-LIVED MOBILE PLATFORM UTILIZING IN-SITU MARTIAN RESOURCES The requirements for performance by planetary exploration missions are increasing. Landing at a single location to take data is no longer sufficient. Due to the increasing cost, the missions that provide mobile platforms that can acquire data at displaced locations are becoming more attractive. Landers have also had limited range due to power limitations, limited lifetime of subsystems and the inability to negotiate rough terrain. The Center for Space Nuclear Research has designed an instrumented platform that can acquire detailed data at hundreds of locations during its lifetime - a Mars Hopper. The Mars Hopper concept utilizes energy from radioisotopic decay in a manner different from any existing radioisotopic power sources—as a thermal capacitor. By accumulating the heat from radioisotopic decay for long periods, the power of the source can be dramatically increased for short periods. Thus, a radioisotopic thermal rocket (RTR) is possible. The platform will be able to “hop” from one location to the next every 5-7 days with a separation of 5-10 km per hop. Each platform will weigh around 50 kgs unfueled which is the condition at deployment. Consequently, several platforms may be deployed on a single launch from Earth. With a lifetime estimated at 5-7 more » years, the entire surface of Mars can be mapped in detail by a couple dozen platforms. In addition, Hoppers can collect samples and deliver them to the Mars Science Laboratory for more detailed analysis. The design and performance of the Mars Hopper will be discussed. « less
Authors: ; ; ;
Publication Date:
OSTI Identifier:OSTI ID: 1004221
Report Number(s):INL/CON-10-19826
TRN: US201103%%471
DOE Contract Number:DE-AC07-05ID14517
Resource Type:Conference
Resource Relation:Conference: International Astronautics Congress,Prague, CZ,09/27/2010,10/01/2010
Research Org:Idaho National Laboratory (INL)
Sponsoring Org:USDOE
Country of Publication:United States
Language:English
Subject: 33 ADVANCED PROPULSION SYSTEMS; DECAY; DESIGN; EXPLORATION; HOPPERS; LIFETIME; PERFORMANCE; ROCKETS mars hopper