Table 9.10
Typical examples of missile-borne auxiliary energy schemes for air defense missiles
Country Serial
number
Model
Type
Main
power
Steering
engine
Auxiliary/primary energy
Characteristic
Russia
1
Sam-2
Middle and
high altitude
Liquid
rocket
engine
Cold air
Power supply: chemical battery;
Gas source: hydraulic unit agent, driving gas
turbine pump to transport propellant;
Cold air source: compressed air, booster
propellant tank; air supply to steering gear I and
II
Multisource,
Comprehensive Utilization,
Constant Power, Excretory
Type
2
Sam-3
Mid-low
altitude
Solid
rocket
engine
Cold air
Cold air source: compressed air, driving air
turbogenerator; air supply to steering gear I, II
Ditto
3
Sam-6
Mid-low
altitude
Solid
impact
engine
Cold air
Ditto
Ditto
U.S.A
4
Tailstock
Ultralow
altitude
portable
Solid
rocket
engine
Electric
Power Supply: Thermal Battery, Power Supply
to Full Bomb Electrical Equipment (Including
Electric Actuator)
Single source,
Comprehensive Utilization,
Common Source, Variable
Power, Excretory
5
Chaparral
Low altitude
Solid
rocket
engine
Gas
Gas Source: Solid Charge Generator, Driving
Gas Turbine Generator; Supply Gas to Steering
Engine
Multisource,
Comprehensive Utilization,
Common Source, Constant
Power, Excretory Type
6
Sparrow
Mid-low
altitude
Solid
rocket
engine
Hydraulic Power supply: solid charge generator, driving
gas turbine generator;
Multisource, individual
settings, source division,
(continued)
108
9 High-Temperature and High-Speed Gas Turbine Pump …