• DocumentCode
    3515555
  • Title

    Aerocapture Technology Development Overview

  • Author

    Munk, Michelle M. ; Moon, Steven A.

  • Author_Institution
    NASA-Langley Res. Center Hampton, Hampton, VA
  • fYear
    2008
  • fDate
    1-8 March 2008
  • Firstpage
    1
  • Lastpage
    7
  • Abstract
    This paper will explain the investment strategy, the role of detailed systems analysis, and the hardware and modeling developments that have resulted from the past 5 years of work under NASA\´s In-Space Propulsion Program (ISPT) Aerocapture investment area. The organizations that have been funded by ISPT over that time period received awards from a 2002 NASA Research Announcement. They are: Lockheed Martin Space Systems, Applied Research Associates, Inc., Ball Aerospace, NASA\´s Ames Research Center, and NASA\´s Langley Research Center. Their accomplishments include improved understanding of entry aerothermal environments, particularly at Titan, demonstration of aerocapture guidance algorithm robustness at multiple bodies, manufacture and test of a 2-meter Carbon-Carbon "hot structure," development and test of evolutionary, high-temperature structural systems with efficient ablative materials, and development of aerothermal sensors that will fly on the Mars Science Laboratory in 2009. Due in large part to this sustained ISPT support for Aerocapture, the technology is ready to be validated in flight.
  • Keywords
    aerospace propulsion; investment; space vehicles; NASA; Titan; aerocapture guidance algorithm; aerothermal environments; aerothermal sensor; arocapture technology; crbon-carbon hot structure; detailed systems analysis; high-temperature structural systems; in-space propulsion program; investment strategy; Aerospace testing; Hardware; IEEE news; Investments; Manufacturing; Materials testing; NASA; Propulsion; Robustness; System testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2008 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-1487-1
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2008.4526545
  • Filename
    4526545