332D 11A
- SIMILAR to 332D-11 but transmits additional pitch and roll attitude information for the radar antenna
- Contains capabilities for fast and normal erection
- Provides monitor signal to indicate proper erection and speed
- Transmits pitch and roll attitude for flight director indicator
- A source of attitude reference information used in integrated flight systems and automatic flight control systems
- Three-wire 400 Hz synchro outputs conforming to ARINC specification are provided in both pitch and roll axes
- Equipment features built-in starting cycle, roll cutout, and monitoring circuits
- Fast erection is automatic during starting
- Both manual recycling and self-testing can readily be provided by appropriate external wiring
DIMMENSIONS |
5 5/8" x 6 3/16" x 7 3/4" |
WEIGHT |
7.2 lbs |
STORAGE TEMPERATURE |
-65C to 70°C |
OPERATING TEMPERATURE |
-54C to 70°C |
AMBIENT HUMIDITY |
0 to 95% |
ALTITUDE |
-1000 to 40 000 feet |
VIBRATION |
5 to 500 Hz at 0.036" double amplitude or 5g |
POWER |
Starting: 60 VA (550 mA at 115 Vac) Running: 35 VA (300 mA at 115 Vac) |
OUTPUT TYPE |
Synchro: 204 mV/degree /-10%, 3-wire, 400 Hz synchro outputs in roll and pitch axes Radar: 51 mV ac/degree /-10%, 2-wire, transformer outputs in pitch and roll axes for radar antenna orientation |
OUTPUT LOADING |
Radar: 10k Maximum for each axis Synchro: Up to three servoed Bendix type AY500-5 synchro control transformers or equivalent plus two 10k resistive load |
NULL VOLTAGE |
40mV maximum no load |
ERECTION CUTOUT |
Internal: 4-9 degress bank External: Provision is made for external cutout, such as external switching rate gyro |
OUTPUT ACCURACY |
more or less 0.5 deg |
ROLL ERECTION CUTOUT |
When bank exceeds 9 degrees |
SYNCHRO ACCURACY |
20 min maximum angular error |
ERECTION RATE |
Normal: 1 to 3 degrees per minute Fast: 5 degrees per minute minimum |
FREE DRIFT |
0.6 Degree per minute maximum |
CONNECTOR |
Bendix Pigmy MS3112E-18-32P Mates with MS3116E-18-32S |