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Castor
Part of Sergeant
American suborbital launch vehicle. Single stage version.
Status: Retired 1982. First Launch: 1967-01-11. Last Launch: 1982-08-04. Number: 9 . Thrust: 235.00 kN (52,830 lbf). Gross mass: 5,200 kg (11,400 lb). Height: 8.00 m (26.20 ft). Diameter: 0.79 m (2.59 ft). Apogee: 300 km (180 mi).
More at: Castor.
Subtopics
| TX-33 Thiokol solid rocket engine. Polaris TV first stage. |
| TX-20 Thiokol solid rocket engine. Draco first stage. |
| TX-30 Thiokol solid rocket engine. Draco second stage. |
| Pollux Thiokol solid rocket engine. Little Joe 1 2P first stage. |
| Castor 30 Solid propellant rocket stage developed for use on space launch vehicles. |
| Castor 1 Thiokol solid rocket engine. Used as apogee kick motor on Delta D, LT Thor Agena D, Scout X-1, Scout X-2, Scout X-3, Scout X-4, TA Thor Agena B, TA Thor Agena D. First flight 1960. M33-20 fourth stage. |
| Castor 2 Thiokol solid rocket engine. Used in Scout A; Delta E; H-1-0; Castor 2. License built in Japan for H-1. First flight 1960. Solid propellant rocket stage. Version for Japanese H-1 booster. |
Family:
suborbital launch vehicle.
Country:
USA.
Launch Sites:
Wallops Island,
Vandenberg,
Poker Flat,
Wallops Island LA4,
Kwajalein,
Kwajalein RN,
Vandenberg 4300C.
Stages:
Castor 1.
Agency:
JPL.
1967 January 11 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 4300C.
Launch Pad: 4300C.
LV Family:
Sergeant.
Launch Vehicle:
Castor.
- Marquardt Scramjet Technology mission - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 54 km (33 mi).
1970 October 9 - .
Launch Site:
Wallops Island.
Launch Complex:
Wallops Island LA4.
LV Family:
Sergeant.
Launch Vehicle:
Castor.
- SPED II re-entry vehicle test flight - .
Nation: USA.
Agency: NASA.
Apogee: 85 km (52 mi).
1975 January 9 - .
Launch Site:
Kwajalein.
Launch Complex:
Kwajalein RN.
LV Family:
Sergeant.
Launch Vehicle:
Castor.
- Re-entry Vehicle test - .
Nation: USA.
Agency: USAF.
Apogee: 200 km (120 mi).
1975 April 13 - .
09:46 GMT - .
Launch Site:
Poker Flat.
LV Family:
Sergeant.
Launch Vehicle:
Castor.
- EXCEDE Active plasma mission - .
Nation: USA.
Agency: USAF.
Apogee: 100 km (60 mi).
1975 August 7 - .
Launch Site:
Kwajalein.
Launch Complex:
Kwajalein RN.
LV Family:
Sergeant.
Launch Vehicle:
Castor.
- Technology mission - .
Nation: USA.
Agency: USAF.
Apogee: 200 km (120 mi).
1975 December 4 - .
Launch Site:
Kwajalein.
Launch Complex:
Kwajalein RN.
LV Family:
Sergeant.
Launch Vehicle:
Castor.
- Technology mission - .
Nation: USA.
Agency: USAF.
Apogee: 200 km (120 mi).
1976 June 27 - .
Launch Site:
Kwajalein.
Launch Complex:
Kwajalein RN.
LV Family:
Sergeant.
Launch Vehicle:
Castor.
- Technology mission - .
Nation: USA.
Agency: USAF.
Apogee: 200 km (120 mi).
1978 December 5 - .
Launch Site:
Kwajalein.
Launch Complex:
Kwajalein RN.
LV Family:
Sergeant.
Launch Vehicle:
Castor.
- DOT 1 Interceptor mission - .
Nation: USA.
Agency: USAF.
Apogee: 235 km (146 mi).
1982 August 4 - .
Launch Site:
Kwajalein.
Launch Complex:
Kwajalein RN.
LV Family:
Sergeant.
Launch Vehicle:
Castor.
- DOT 5 - .
Nation: USA.
Agency: USAF.
Apogee: 230 km (140 mi).
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