637672

Aircraft attitude computer

637672 Description

Base, shock mount mounting type, an/asn-56 inertial navigation sys; rf4c aircraft end item identification, 23.600 inches unpackaged unit length.

Features

Additional information computed: climb angle, vertical velocity, ground speed to altitude ratio

Properties of 637672

Mounting Type:
Base, shock mount
End Application:
An/asn-56 inertial navigation sys; rf4c aircraft
Unpackaged Unit Length:
23.600 inches
Unpackaged Unit Width:
4.250 inches
Unpackaged Unit Height:
9.740 inches
Power Source:
External
Input Intelligence Type:
Altitude, general data and ground speed and pitch-roll signal data
Intelligence Input Method:
Electrical
Output Intelligence Type:
Angle of attack
Functional Description:
Contains the follow-up servos for pitch and roll information from the inertial navigation set stable platform, and circuitry for computing vertical attack angle, climb angle, vertical velocity, and ground speed to altitde ratio
Reference Data And Literature:
Tech order 5n16-2-6-4 and dd form 61
Relationship To Similar Equipment:
REPL-AC-ES6-6050
Type/model Designation:
Cp-780/asn-56
NSN:
6605-00-915-9319
Description:
Computer,aircraft Attitude
Cage Code:
1XSM7

Definition Aircraft Attitude Computer

A computer that contains the follow-up servo for pitch and roll information from the platform, and the circuitry for computing vertical attack angles, climb angle, vertical velocity, and ground speed to altitude ratio.

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Last modified 05/16/2024