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Source: The Open Library

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1An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5

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“An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5” Metadata:

  • Title: ➤  An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information
  • Publish Date:
  • Publish Location: Hampton, Va - Hanover, MD

“An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 2001
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

Online Access

Downloads Are Not Available:

The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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    2Inviscid flow computations of several aeroshell configurations for a '07 Mars lander

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    “Inviscid flow computations of several aeroshell configurations for a '07 Mars lander” Metadata:

    • Title: ➤  Inviscid flow computations of several aeroshell configurations for a '07 Mars lander
    • Author:
    • Language: English
    • Publisher: ➤  Available from NASA Center for Aerospace Information - National Aeronautics and Science Administration, Langley Research Center
    • Publish Date:
    • Publish Location: Hampton, Va - Hanover, MD

    “Inviscid flow computations of several aeroshell configurations for a '07 Mars lander” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 2001
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Access

    Downloads Are Not Available:

    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

    Online Borrowing:

      Online Marketplaces

      Find Inviscid flow computations of several aeroshell configurations for a '07 Mars lander at online marketplaces:


      3Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24

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      “Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24” Metadata:

      • Title: ➤  Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24
      • Author:
      • Language: English
      • Publisher: ➤  Available from NASA Center for Aerospace Information - National Aeronautics and Science Administration, Langley Research Center
      • Publish Date:
      • Publish Location: Hampton, Va - Hanover, MD

      “Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 2001
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

      Online Access

      Downloads Are Not Available:

      The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

      Online Borrowing:

        Online Marketplaces

        Find Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24 at online marketplaces:


        4Superalloy foams for aeroshell applications

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        “Superalloy foams for aeroshell applications” Metadata:

        • Title: ➤  Superalloy foams for aeroshell applications
        • Author:
        • Language: English
        • Publisher: ➤  Available from NASA Center for AeroSpace Information - National Aeronautics and Space Administration, Glenn Research Center
        • Publish Date:
        • Publish Location: Cleveland, Ohio - Hanover MD

        “Superalloy foams for aeroshell applications” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 2001
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

        Online Access

        Downloads Are Not Available:

        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

        Online Borrowing:

          Online Marketplaces

          Find Superalloy foams for aeroshell applications at online marketplaces:



          Wiki

          Source: Wikipedia

          Wikipedia Results

          Search Results from Wikipedia

          Aeroshell

          dynamics of aeroshells are influenced by inertial and drag forces, as defined it this equation: ß=m/CdA where m is defined as the mass of the aeroshell and its

          Pioneer Venus project

          targeted at different parts of the planet; They had no parachutes and the aeroshells did not separate from the probe. Two of the small probes reached the surface

          Atmospheric entry

          Pathfinder and Mars Exploration Rover (MER) aeroshells. The BIP was at the attachment points between the aeroshell's backshell (also called the afterbody or

          Voyager program (Mars)

          landers would have been Surveyor moon probes modified with the use of aeroshells and a combination parachute/retrorocket landing systems. Funding for the

          Aerocapture

          and atmospheric guidance techniques have shown that heritage low-L/D aeroshells such as Apollo offer sufficient control authority for aerocapture at Neptune

          Mars Exploration Rover

          Colorado, the aeroshell is made of an aluminium honeycomb structure sandwiched between graphite-epoxy face sheets. The outside of the aeroshell is covered

          Alaska Airlines Flight 261

          manufacturer McDonnell Douglas) of Aeroshell 33 grease instead of the previously approved lubricant, Mobilgrease 28. The use of Aeroshell 33 was found not to be a

          Crack the Skye

          we've previously recorded in the sense that we kinda strapped on our aeroshells and departed from Earth for a while, and then captained to the ethereal

          Viking program

          above the surface by the extended legs. Each lander was enclosed in an aeroshell heat shield designed to slow the lander down during the entry phase. To

          EAA AirVenture Oshkosh

          Aeroshell Aerobatic Team performing at EAA AirVenture 2007