Detecting-Ranging Set AN/AAS-33A

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Detecting-Ranging Set AN/AAS-33A

Detecting-Ranging Set AN/AAS-33A
Referenced Documents
Issues of documents-cont.
Issues of documents-cont.
Issues of documents-cont.
Microelectronic modular assemblies
Subassembly finishes
Table 1. Time totalizing meters
Cabling and connections
Operation of controls
Organizational level maintenance
Built-in-test (BIT)
Fault isolation test (FIT) requirements
Weapon replaceable assembly (WRA)
Adjustments and alignments
Table 2. Standard conditions
Table 4. Temperature, aircraft compartments
Primary input power requirements
Cooling method for equipment
Hydraulic system requirements
RG overboard drain
Servomotor design and performance requirements
Protection of ground personnel during organizational maintenance
Operating modes
Turret, stabilized platform (TSP)
Turret assembly
Electronic control amplifier (ECA)
Gyro driver and oscillator assembly
Gimbal angle indicators
Display interfaces
Operating modes
Housing and optics
Zoom assembly
Automatic responsivity control narcissus assembly (ARC/NARC)
Preamp multiplexer circuit board assemblies
Compressor, reciprocating
Electron tube assembly
Mode logic and sweep fail module
Slow sweep and video module
L-PRF light
Receiver-Transmitter, Laser (LRT), Generator-Processor (LTE), and Assembly, Cable (PFN Cable)
Designate (DES) mode
Forward optics assembly
Logic assembly
PFN power supply assembly
Receiver, laser (FAC RCVR), and processor, signal (LRE)
Video processor assembly
Power supply (LVPS)
15 VDC linear regulators
DRS power and operating modes
Laser transmit modes
Chassis subassembly
Temperature controller logic
Manufacturing reliability screening
Card conditioning (non-operating) thermal
Manufacturing run-in (MRI) test
Reliability assurance tests
Nonrelevant failures
Reconditioning of equipment under test
Performance objectives
List of acronyms or abbreviations
List of acronyms or abbreviations-cont.
Definitions
Optical reference line (ORL)
Figure 1. Random vibration spectrum, receiver group
Figure 2. Random vibration spectrum, group II WRAs
Figure 3. Flight vibration envelope, receiver group
Figure 4. Receiver group operating envelope
Figure 5. Gyro warm-up time
Figure 6. Maximum airload and pressure distribution
Figure 7. Reference markers
Figure 8. Reticle characteristics
Specification Analysis Sheet
Postage and Fees Paid

Detecting-Ranging Set AN/AAS-33A

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