Castor 2
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
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.
Thrust (sl): 229.300 kN (51,549 lbf). Thrust (sl): 23,379 kgf. Area Ratio: 7.45.
Related
- Country
- USA
- Launch Vehicles
- Scout A, Blue Scout Junior, Blue Scout I, Blue Scout II, Blue Scout Jr SLV-1C, Scout B, Thor Delta E, Scout B 2A, Thor Delta E1, Scout X-5C, Thor Delta J, Thor Delta N, Thor Delta M, Thorad SLV-2H Agena D, Thor Delta L, Thor Delta N6, Thor Delta M6, Scout B-1, Scout B-1 F, Delta 0900, Scout D-1, Delta 1604, Delta 0300, Strypi VIIAR, Delta 1914, Scout D-1 F, Delta 1913, Scout A-1, Delta 1900, Delta 2313, Strypi IIAR, Delta 2914, Scout E-1, Delta 2310, Delta 2910, Delta 1410, Scout F-1, Delta 1910, Delta 2913, N-1, Scout G-1, N-2, N-2 (2), Delta 0100, Scout D, H-1, H-1 (2), H-1 6R, Advanced Scout
- Propellants
- Solid
- Stages
- Castor 2
- Agency
- Thiokol