American suborbital launch vehicle. Three stage vehicle consisting of 1 x Algol 2B + 1 x Castor 2 + 1 x Antares 2
AKA: Scout X-5C.
More... - Chronology...
Gross mass: 17,500 kg (38,500 lb).
Height: 22.00 m (72.00 ft).
Diameter: 1.02 m (3.34 ft).
Thrust: 380.00 kN (85,420 lbf).
Apogee: 180 km (110 mi).
First Launch: 1968.04.27.
Number: 1 .
Scout Solid-fuel, light payload, lower-cost launch vehicle developed by the Air Force and NASA in the late 1950's and used in a variety of configurations over thirty years. Launched from Cape Canaveral, Vandenberg, Wallops Island, and from Italy's equatorial San Marco platform off Kenya. Italy studied but did not develop subsequent upgraded versions. More...
Associated Manufacturers and Agencies
Vought American manufacturer of rockets and spacecraft. Vought, USA. More...
Associated Launch Sites
Wallops Island Small NASA launch site for sounding rocket launches and occasional Scout launches to orbit. Air launches are conducted from the Drop Zone Wallops Island, 37.00 N 72.0 W. With the last orbital launch in 1985 and the decline in sounding rocket launches, Wallops fell into near-disuse as a launch center. Its fortunes revised with the establishment of Mid-Atlantic Regional Spaceport in 2005 and orbital launches resumed in 2010. More...
Algol 2B Solid rocket stage. 400.00 kN (89,924 lbf) thrust. Mass 10,700 kg (23,589 lb). More...
Antares 2 Solid propellant rocket stage. Loaded/empty mass 1,400/300 kg. Thrust 93.09 kN. Vacuum specific impulse 293 seconds. More...
Castor 2 Solid propellant rocket stage. Loaded/empty mass 4,424/695 kg. Thrust 258.92 kN. Vacuum specific impulse 262 seconds. More...
Scout X-5 Chronology
1968 April 27 -
05:19 GMT - .
: Wallops Island
. Launch Complex
: Wallops Island LA3A
. LV Family
. Launch Vehicle
: Scout X-5
. LV Configuration
: Scout X-5C S164C.
- Reentry 5 re-entry vehicle test flight - .
Nation: USA. Agency: NASA. Apogee: 175 km (108 mi).
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