Winston
Lorenzo von Matterhorn
- Joined
- Jan 31, 2009
- Messages
- 9,559
- Reaction score
- 1,732
The largest diameter solid rocket motor ever made and the highest thrust rocket motor of any kind ever made. Propellant burned at 6 tons per second rate. It took three months around the clock to fill with propellant using many small batches; elevated temperature cured for three weeks; cooled for two weeks. After the mandrel was withdrawn technicians were lowered into the core to inspect for defects. The SL-3 test produced over 5 million pounds of thrust.
Thrust: 17,695.30 kN (3,978,062 lbf)
Gross mass: 831,345 kg (1,832,801 lb)
Unfuelled mass: 85,321 kg (188,100 lb)
Specific impulse: 263 s
Specific impulse sea level: 238 s
Burn time: 114 s.
Height: 18.29 m (60.00 ft)
Diameter: 6.60 m (21.60 ft)
Exhaust candlepower: 3 million
https://www.astronautix.com/a/aj-260-2.html
https://nasawatch.com/archives/2015/03/nasa-forgot-the.html
GREAT video overview of manufacture and firing:
https://youtu.be/o4BkDQjM2Jc?t=22m4s
Thrust: 17,695.30 kN (3,978,062 lbf)
Gross mass: 831,345 kg (1,832,801 lb)
Unfuelled mass: 85,321 kg (188,100 lb)
Specific impulse: 263 s
Specific impulse sea level: 238 s
Burn time: 114 s.
Height: 18.29 m (60.00 ft)
Diameter: 6.60 m (21.60 ft)
Exhaust candlepower: 3 million
https://www.astronautix.com/a/aj-260-2.html
https://nasawatch.com/archives/2015/03/nasa-forgot-the.html
GREAT video overview of manufacture and firing:
https://youtu.be/o4BkDQjM2Jc?t=22m4s







