Table 9.10
(continued)
Country Serial
number
Model
Type
Main
power
Steering
engine
Auxiliary/primary energy
Characteristic
Gas source: solid charge generator, gas
supercharged accumulator, guide antenna for
fuel supply;
Cold air source: nitrogen, booster accumulator,
oil supply to steering gear
variable power, excretory
type
7
Standard
Medium-range
ship-to-air
Solid
rocket
engine
Electric
Same as Tailstock
Same as Tailstock
8
Patriot
Medium and
Long Range
Solid
rocket
engine
Hydraulic Power supply: One battery supplies power to
the generator, drives the variable displacement
pump to supply oil to the steering gear, and the
other battery supplies power to other electrical
equipment on the missile.
Cold air source: helium, pressurize the tank
before pump, inflate the gas–liquid accumulator
Multisource, individual
settings, source division,
variable power, cyclic
Britain
9
Sea Javelin Medium-range
ship-to-air
Ramjet Hydraulic Power supply: thermal battery;
Gas Source: Liquid Unit Agent, Gas
Supercharged Fuel Tank; Drive Gas Motor
Variable Pump, Supply Oil to Steering
Engine I, II
Multisource,
comprehensive utilization,
common source, variable
power, cyclic
France
10
Rattlesnake Low altitude
Solid
rocket
engine
Electric
Power supply: Battery, power supply to
all-missile electrical equipment (including
electric steering gear)
Single source,
comprehensive utilization,
common source, variable
power, excretory
Italy
11
Aspide
Mid-low
altitude,
General
purpose of the
Army
Solid
rocket
engine
Hydraulic Gas Source: Solid Charge Generator, which
supplies gas to turbine and drives generator and
hydraulic pump at the same time. Power supply
to the whole missile and oil supply to the
hydraulic steering gear and seeker, respectively
Multisource, individual
settings, source division,
constant power, cyclic
9.1 Electro-Hydraulic Servo Control Technology of Aircraft Gas Turbine Pump
109