FG-02
The FG-02 was a Chinese solid rocket motor burning Polysulfide. It was developed by (also known as the 6th Academy of CASIC) for use in the Long March 1 third stage. It has a total nominal mass of 2,052 kg (4,524 lb), of which 1,806 kg (3,982 lb) is propellant load. It has an average thrust of 118 kN (27,000 lbf) with a specific impulse of 254 seconds burning for 38 seconds, with a total impulse of 4,500 kN (1,000,000 lbf). It used spin stabilization and a timing device to ignite in flight.
FG-02
The FG-02 was a Chinese solid rocket motor burning Polysulfide. It was developed by (also known as the 6th Academy of CASIC) for use in the Long March 1 third stage. It has a total nominal mass of 2,052 kg (4,524 lb), of which 1,806 kg (3,982 lb) is propellant load. It has an average thrust of 118 kN (27,000 lbf) with a specific impulse of 254 seconds burning for 38 seconds, with a total impulse of 4,500 kN (1,000,000 lbf). It used spin stabilization and a timing device to ignite in flight.
has abstract
The FG-02 was a Chinese solid ...... March 3, 1971, on the mission.
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Wikipage page ID
47,360,936
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Wikipage revision ID
1,000,693,377
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associated
burn time
combustion chamber
country of origin
first date
1970-04-24
fuel
last date
1971-03-03
name
FG-02
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purpose
Upper stage
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status
Retired
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type
solid
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used in
wikiPageUsesTemplate
hypernym
comment
The FG-02 was a Chinese solid ...... ng device to ignite in flight.
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label
FG-02
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