1.8KS7800
From Infogalactic: the planetary knowledge core
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Country of origin | United States |
---|---|
Date | 1957 |
Designer | Aerojet |
Status | Retired |
Solid-fuel motor | |
Performance | |
Thrust (vac.) | 35 kN |
Dimensions | |
Length | 1.3 m |
Diameter | 0.2 m |
1.8KS7800 is a solid propellant rocket engine designed by Aerojet and used in the AIM-7A, AIM7B and AIM7C Sparrow missiles.[1] The designation 1.8KS7800 means that the engine burns during 1.8 seconds and generates 7,800 pounds of thrust.[2][3][4]
References
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