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  • 1
    Publication Date: 2019-07-13
    Description: NASA has been investigating potential translunar excursion concepts to take place in the 2020s that would be used to test and demonstrate long duration life support and other systems needed for eventual Mars missions in the 2030s. These potential trajectory concepts could be conducted in the proving ground, a region of cislunar and near-Earth interplanetary space where international space agencies could cooperate to develop the technologies needed for interplanetary spaceflight. Enabled by high power Solar Electric Propulsion (SEP) technologies, the excursion trajectory concepts studied are grouped into three classes of increasing distance from the Earth and increasing technical difficulty: the first class of excursion trajectory concepts would represent a 90-120 day round trip trajectory with abort to Earth options throughout the entire length, the second class would be a 180-210 day round trip trajectory with periods in which aborts would not be available, and the third would be a 300-400 day round trip trajectory without aborts for most of the length of the trip. This paper provides a top-level summary of the trajectory and mission design of representative example missions of these three classes of excursion trajectory concepts.
    Keywords: Lunar and Planetary Science and Exploration; Astrodynamics
    Type: GRC-E-DAA-TN27479 , IEEE Aerospace Conference 2016; Mar 05, 2016 - Mar 12, 2016; Big Sky, MT; United States
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  • 2
    Publication Date: 2019-07-13
    Description: Advances in solar array and electric thruster technologies now offer the promise of new, very capable space transportation systems that will allow us to cost effectively explore the solar system. NASA has developed numerous solar electric propulsion spacecraft concepts with power levels ranging from tens to hundreds of kilowatts for robotic and piloted missions to asteroids and Mars. This paper describes nine electric and hybrid solar electric/chemical propulsion concepts developed over the last 5 years and discusses how they might be used for human exploration of the inner solar system.
    Keywords: Lunar and Planetary Science and Exploration; Spacecraft Propulsion and Power
    Type: E-19129 , GRC-E-DAA-TN25991 , Space 2015; Aug 31, 2015 - Sep 02, 2015; Pasadena, CA; United States
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  • 3
    Publication Date: 2019-07-19
    Description: NASA continues to advance plans to extend human presence beyond low-Earth orbit leading to human exploration of Mars. The plans being laid out follow an incremental path, beginning with initial flight tests followed by deployment of a Deep Space Gateway (DSG) in cislunar space. This Gateway, will serve as the initial transportation node for departing and returning Mars spacecraft. Human exploration of Mars represents the next leap for humankind because it will require leaving Earth on a long mission with very limited return, rescue, or resupply capabilities. Although Mars missions are long, approaches and technologies are desired which can reduce the time that the crew is away from Earth. This paper builds off past analyses of NASA's exploration strategy by providing more detail on the performance of alternative in-space transportation options with an emphasis on reducing total mission duration. Key options discussed include advanced chemical, nuclear thermal, nuclear electric, solar electric, as well as an emerging hybrid propulsion system which utilizes a combination of both solar electric and chemical propulsion.
    Keywords: Lunar and Planetary Science and Exploration; Spacecraft Propulsion and Power
    Type: JSC-CN-40290 , Annual IEEE Aerospace Conference 2018; Mar 03, 2017 - Mar 10, 2017; Big Sky, MT; United States
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