Box 17
Contains 12 Results:
Department 3257, 1960-1962
Includes: simulator aircraft, coupler card assembly, flight director computer/CPU-27/A, Z-5 computer, vibration analyzer, turbine vibration indicator and analyzer, flight data computer, and parallel actuator.
Department 3257, 1963-1964
Includes: vibration analyzer, test setup for RF interference, universal altitude indicator, flight director computer, STEVI, consolidated system configuration take for STEVI, and field test setup.
Department 3261, 1945-1951
Includes: subminiature amplifier, all weather flight control, scorsby fundamental gyro study, and horizon compass repeater.
Department 3261, 1952-1954
Includes: transistor motor amplifier, miniaturized A-12 auto pilot, A-5 altitude flight control sine wave generator and accelerometer, bearing cap, basic safety system test equipment, loading fixture servo boost activator, A-12 D boost valve pickoff, A/S control amplifier and miniaturized A-12 comp., pickup unit electric boost control, beam guidance modulator test jig unit, A-12 beam guidance control system.
Department 3261, 1955-1956
Includes: A-14 flight controller analyzer, rate gyros, radio coupler and rate gyro, A-15 servo vibration test, autopilot indicator, SP-30 servo system and amplifier, control wheel SP-30, proportional disconnect control wheels, signal generator, and A-12 amplifiers/experimental.
Department 3261, 1957
Includes: acceleration test machine transmitter, SP-30 UG test setup, vibration test machine transmitter, stab rack and flight control computer, SP-30, shock test, vibration test truck pit shock test, altitude and cruise computer mount resilient computer, shock test mount kes machine transmitter, test setup for altitude and cruise computer machine transmitter, SP-30 servo motor salt spray and salt test, SP-30 servo motor assembly in vibration temperature chamber, SP-30 indicator shock test, AFCS controller, safety monitor, SP-30 vertical gyro, flight control computer and stabilizer rack, amplifier assembly, SP-30 servo bracket, and servo assembly.
Department 3261, 1958-1960
Includes: setup for SP-30 auto pilot, A2F control computer shock and vibration, radio coupler, flight control computer, environmental test, SP-30 stabilization computer, SP-30 flight control computer, oscillograph, gyro precession, loading fixture, stabilization computer, vibration test stabilization computer, control wheel transducer, turn control assembly, SP-30 pressure computer, control stitch transducer, simplified beam coupler, salt spring test, amplifier detection assembly, alias coupler, acceleration test, AFCS controller, and back assembly and servo amplifier.
Department 3262, 1954-1955
Includes: vertical gyro, A-14 auto pilot servo cut-out system, pedestal controller, and command selector.
Department 3262, 1956
Includes: A-14 test fixtures, latitude corrected yove gyro, A-14 amplifier assembly test fixture, A-14 line analyzer, explosion proof test text fixture, A/S mach. system components, silicone diode transistor amplifier, A-14 servo motor drive drum and bracket, A-12 auto pilot test fixture and dynameter, and vibration test fixture.
Department 3262, 1958-1962
Includes: sequential timer and tantalum capacitor test setup, AFCS controller, vibration test of AIP indicator, Doppler radar, and INFPC air data computer.
Department 3262, 1952-1954
Includes: helicopter auto pilot, integrator amplifier auto pilot, miniature amplifier assembly automatic pilot, S-55 helicopter, remote rate gyro, helicopter flight instrument components, and helicopter rotor speed control and flight director.
Department 3263, 1955-1958
Includes: sonar control, pre-amplifier AQS-4 mod. rid accelerometer, signal demodulators, air data computer, roll rate damper control A-14 test equipment, H2-1 D, component hydraulic lab, diode test equipment, differential linkage assembly, manual flight system lab mockup, helicopter differential control linkage, electronic preamplifier and magnetic amplifier, and H-3 command pickoff.