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Source: The Open Library

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1Affordable In-Space Transportation

“Affordable In-Space Transportation” Metadata:

  • Title: ➤  Affordable In-Space Transportation
  • Language: English
  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Marshall Space Flight Center
  • Publish Date:
  • Publish Location: MSFC, Ala - [Springfield, Va

“Affordable In-Space Transportation” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1996
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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    Solid-propellant rocket

    space probes. Solids are, however, frequently used as strap-on boosters to increase payload capacity or as spin-stabilized add-on upper stages when higher-than-normal

    Star (rocket stage)

    family of US solid-propellant rocket motors originally developed by Thiokol and used by many space propulsion and launch vehicle stages. They are used

    Altair (rocket stage)

    The Altair was a solid-fuel rocket with a fiberglass casing, initially developed for use as the third stage of Vanguard rockets in 1959. It was manufactured

    List of artificial objects leaving the Solar System

    Pioneer 11 are now derelict. In addition to these spacecraft, some upper stages and de-spin weights are leaving the Solar System, assuming they continue on

    Spinning wheel

    A spinning wheel is a device for spinning thread or yarn from fibres. It was fundamental to the textile industry prior to the Industrial Revolution. It

    Star 48

    largest of a family of solid rocket motors used by many space propulsion and launch vehicle stages, almost exclusively as an upper stage. It was developed

    Ares I-X

    consisted of a functional four-segment solid rocket booster (SRB) stage, a fifth segment mass simulator, an upper-stage simulator (USS), which was similar

    Juno I

    with an acceleration of 25–51 g. The tub along with the fourth stage were set spinning while the launch vehicle was on the launch pad to provide gyroscopic

    Juno II

    stage. Solid-fueled rocket motors derived from the MGM-29 Sergeant were used as upper stages, eleven for the second stage, three for the third stage,

    Jupiter-C

    consisted of a modified Redstone ballistic missile with two solid-propellant upper stages. The tanks of the Redstone were lengthened by 8 ft (2.4 m) to