Status: Retired 1968. First Launch: 1967-07-25. Last Launch: 1968-11-09. Number: 8 . Gross mass: 25,000 kg (55,000 lb). Height: 15.10 m (49.50 ft). Diameter: 1.50 m (4.90 ft). Apogee: 500 km (310 mi).
2 stage vehicle consisting of 1 x SEP 901 + 1 x SEP 903.
SEP 903 SEP solid rocket engine. SSBS S01 second stage. |