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CA1100463A
|
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Nozzle structure with notches
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GB1186393A
|
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Mass Flow Control
|
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US3432123A
|
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Cross ducting system for augmentor wing aircraft
|
|
GB1080013A
|
|
Improvements in or relating to mass flow measuring apparatus
|
|
GB1076163A
|
|
Improvements in or relating to moisture-extracting devices
|
|
GB1116801A
|
|
Improvements in or relating to homing systems
|
|
GB1070723A
|
|
Improvements in or relating to aircraft
|
|
GB1068347A
|
|
Improvements in or relating to control systems
|
|
GB1042140A
|
|
Improvements in or relating to pulse train generators
|
|
GB1068346A
|
|
Improvements in or relating to frequency comparison devices
|
|
US3289183A
|
|
Multi-directional shifting device
|
|
US3153341A
|
|
Rotary fluid flowmeter sensing element
|
|
GB1047011A
|
|
Improvements in or relating to manual control members
|
|
US3153322A
|
|
Magnetic amplifier circuits
|
|
US3213288A
|
|
Magnetic amplifier engine control system
|
|
GB1021544A
|
|
Improved variable pitch propeller control system
|
|
US3093350A
|
|
Aircraft wing with nose flap and boundary layer control
|
|
GB977030A
|
|
Improvements in or relating to encapsulating articles
|
|
GB963268A
|
|
Improvements in or relating to apparatus for detecting low frequency alternating current
|
|
GB1511642A
|
|
Optical systems for missile fuses
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