• DocumentCode
    3206659
  • Title

    Mars Ascent Vehicle technology planning

  • Author

    Dankanich, John W.

  • Author_Institution
    Gray Res., Inc., Cleveland, OH
  • fYear
    2009
  • fDate
    7-14 March 2009
  • Firstpage
    1
  • Lastpage
    9
  • Abstract
    For many years, NASA and the science community have been asking for a Mars sample return (MSR) mission. There have been numerous studies to evaluate MSR mission architectures, technology needs and development plans, and top-level requirements. Because of the challenges, technologically and financially, of the MSR mission, NASA initiated a study to look at MSR propulsion technologies through the In-Space Propulsion Technology (ISPT) project office. The objective of the ISPT project is to develop propulsion technologies that enhance or enable NASA science missions, specifically for the planetary science division, by increasing performance while reducing cost, risk, and/or trip times. The largest propulsion risk element of the MSR mission is the Mars ascent vehicle (MAV). In preparation for the procurement of the MAV system development and flight tests, a survey of the propulsion options was conducted and a technology development approach has been established. The results of the MAV system trades and development plan are presented.
  • Keywords
    Mars; aerospace propulsion; space vehicles; In-Space Propulsion Technology project office; MSR propulsion technology; Mars ascent vehicle; Mars ascent vehicle technology planning; Mars sample return mission; NASA science mission; planetary science division; Costs; Earth; Mars; NASA; Procurement; Propulsion; Space technology; System testing; Technology planning; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace conference, 2009 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    978-1-4244-2621-8
  • Electronic_ISBN
    978-1-4244-2622-5
  • Type

    conf

  • DOI
    10.1109/AERO.2009.4839592
  • Filename
    4839592