enow.com Web Search

  1. Ad

    related to: orion solid rocket motors

Search results

  1. Results from the WOW.Com Content Network
  2. Orion (rocket stage) - Wikipedia

    en.wikipedia.org/wiki/Orion_(rocket_stage)

    Orion is a series of American solid-fuel rocket stages, developed and manufactured by a joint venture between Hercules Aerospace and Alliant Techsystems (now Northrop Grumman Innovation Systems). They were originally developed for use as all three stages on the Pegasus rocket , first flown in 1990.

  3. Terrier Orion - Wikipedia

    en.wikipedia.org/wiki/Terrier_Orion

    The Terrier Orion system is designed to be rail launched, and can be supported at most fixed and mobile launch sites. [2] The Terrier Mk 12 Mod 1 or Mk 70 rocket used for the first stage uses an 18-inch (46 cm) diameter motor along with 2.5-or-4.8-square-foot (0.23 or 0.45 m 2) cruciform configured tail fins. The Improved Orion motor used in ...

  4. Nike (rocket stage) - Wikipedia

    en.wikipedia.org/wiki/Nike_(rocket_stage)

    The Nike Tomahawk has a Nike rocket as the first stage, and a Tomahawk rocket as the second. The Nike Tomahawk has a ceiling of 230 statute miles (370 km), a payload capacity of 100 pounds (45 kg), a launch thrust of 49,000 pounds of force (217 kN ), a launch weight of 2,200 pounds (1,000 kg), a diameter of 17 inches (0.43 m) and a length of 35 ...

  5. Northrop Grumman Pegasus - Wikipedia

    en.wikipedia.org/wiki/Northrop_Grumman_Pegasus

    The tail fins provide steering for first-stage flight, as the Orion 50S motor does not have a thrust-vectoring nozzle. Approximately 1 minute and 17 seconds later, the Orion 50S motor burns out. The vehicle is at over 200,000 feet (61 km) in altitude and hypersonic speed. The first stage falls away, taking the wing and tail surfaces, and the ...

  6. Orion (rocket) - Wikipedia

    en.wikipedia.org/wiki/Orion_(rocket)

    Orion, using a Aerojet M22E8 dual-thrust motor (from the MIM-23A Hawk missile). Improved Orion using a Aerojet M112 dual-thrust motor (from the MIM-23B I-Hawk missile). The sounding rocket is launched from Wallops Flight Facility, White Sands , Poker Flat Rocket Range , Andoya Rocket Range , Esrange and Barreira do Inferno .

  7. Tekoi - Wikipedia

    en.wikipedia.org/wiki/Tekoi

    Tekoi Rocket Test Range, or Tekoi, is a former solid fuel rocket motor test and calibration site operated by Hercules Aerospace near the Utah Test and Training Range in Utah's West Desert, approximately 80 miles (130 km) west of Salt Lake City, Utah. It is located on the Goshute's Skull Valley Indian Reservation.

  8. AJ10 - Wikipedia

    en.wikipedia.org/wiki/AJ10

    It was used by the Delta-F upper stage of the Delta 1000 Straight Eight series rocket, starting in 1972. This version also used Aerozine 50 as fuel and nitrogen tetroxide (N 2 O 4 ) as oxidizer. The AJ10-190 engine was used on the Space Shuttle Orbital Maneuvering System (OMS) for orbital insertion, on-orbit maneuvers, and de-orbiting, first ...

  9. Comparison of solid-fuelled orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_solid...

    Solid Liquid LEO Other orbit Ares I: 1 1 United States: Alliant Techsystems / Boeing: 94 5.5 25000 (2015) 0/0 Cancelled Athena I: 2 1 United States: Lockheed Martin: 1995 2001 3/4 Retired Athena Ic: 2 1 United States: Lockheed Martin Alliant Techsystems (2012) 0/0 Development Athena II [7] 3 1 United States: Lockheed Martin: 30.5 2.36 120.2 ...

  1. Ad

    related to: orion solid rocket motors