American target missile. Four stage vehicle consisting of 2 x Recruit + 1 x Castor + 1 x Alcor IB + 1 x Alcyone
Gross mass: 4,600 kg (10,100 lb).
Height: 11.20 m (36.70 ft).
Diameter: 0.79 m (2.59 ft).
Thrust: 499.00 kN (112,179 lbf).
Apogee: 170 km (100 mi).
First Launch: 1975.03.11.
Last Launch: 1975.09.18.
Number: 2 .
More... - Chronology...
Associated Countries
See also
-
Strypi Family of re-entry vehicle test boosters and anti-missile targets using a Castor first stage with two recruit strap-ons, plus a range of upper stages. More...
-
missile Guided self-propelled military weapon (as opposed to rocket, an unguided self-propelled weapon). More...
Associated Manufacturers and Agencies
-
Sandia American manufacturer of rockets and spacecraft. Sandia Laboratories, Albequerque, 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...
Associated Stages
-
Alcor IB Solid rocket stage. 42.00 kN (9,442 lbf) thrust. Mass 500 kg (1,102 lb). More...
-
Alcyone Solid rocket stage. 34.00 kN (7,644 lbf) thrust. Mass 100 kg (220 lb). More...
-
Castor 1 Solid propellant rocket stage. Loaded/empty mass 3,852/535 kg. Thrust 286.00 kN. Vacuum specific impulse 247 seconds. More...
Strypi VIIR Chronology
1975 March 11 - .
Launch Site:
Wallops Island.
LV Family:
Strypi.
Launch Vehicle:
Strypi VIIR.
- MTV-II-2 re-entry vehicle test flight - .
Nation: USA. Agency: Sandia. Apogee: 170 km (100 mi).
1975 September 18 - .
Launch Site:
Wallops Island.
LV Family:
Strypi.
Launch Vehicle:
Strypi VIIR.
- NRV Nosetip Recovery Re-entry vehicle test - .
Nation: USA. Agency: Sandia. Apogee: 170 km (100 mi).
Home - Browse - Contact
© / Conditions for Use