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F-5 HUD PDU (space model)

Technical Information

Catalogue No: C0449
Category: Head-Up Display [HUD]
Object Type: Model
Object Name: F-5 HUD PDU (space model)
Part No: None
Serial No: None
Manufacturer: Unknown
Division: Unknown
Platform(s): F-5
Year of Manufacture: circa 1990
Dimensions: Width (mm): 140
Height (mm): 290
Depth (mm): 690
Weight (g): 5,880
Location: Main Store
Inscription(s):

None

Notes:

This is a model of a HUD with a great similarity to that fitted on the Thai F-5E/F programme. It may have been used as an installation fit model or simply as a demonstrator for similar programmes.

The RAA contains a number of models of equipment and aircraft. The equipment models were used as a marketing aid and often to ensure that the production unit will fit in the space; this was particularly true for Head Up Displays. Such equipment models will have minimal or no functionality. Models might  just be used as weighted units or as cockpit lighting evaluation units. The HUD used on the YF-16 was of the correct weight and envelope but only mounted the Spin 'chute button (a feature only required for the early test flights). Many of these models were made by professional model makers from the original drawings and could be quite expensive; alternatively the real hardware would be used.

The aircraft models range from the simple small scale kits to quite large display items. The large model aircraft were often a marketing tool from places like Airbus or Boeing but may be found in Boardrooms or Reception areas wheras the small models may be given as a visitor handout. Those models made from kits have largely been brought in from home but are useful to illustrate the platform alongside the equipment. The large models will be hugely expensive.

The F-5 was sold to many countries and provided a simple but effective fighter aircraft with potential for avionic upgrade. The Company worked on various upgrade programmes and in each case a replacement for the existing  Lead Computing Optical Sight (LCOS) was offered.

The earliest such replacement is seen in Catalogue No. C0022. The HUDWAC consists of three line replaceable units; the Pilot’s Display Unit (PDU), an Electronics Unit (EU) and a Weapon Data Input Panel (WDIP).

The physical configuration of the HUDWAC was designed to be drop-in compatible with all known versions of the F-5E/F. Other than removal of the Lead Computing Optical Sight (LCOS) no rearrangement of existing systems nor structural modification was necessary; the new PDU mounts onto the same LCOS tray. The HUDWAC was made to be interchangeable between F-5E’s fitted with the APQ-153 radar and AHRS and those fitted with an APQ-159 radar and an INS without any modifications. The HUDWAC monitors the armament panel switch settings and the in-built software determines the required operating mode which overall makes the system easier to use than the original LCOS.

The PDU gives a field of view nearly twice that of the ASG-29 Lead Computing Optical Sight it replaces. The unit hosts a control panel with switches and a keypad through which mission data such as target elevation and barometric pressure can be loaded. A 16mm film camera or a colour video camera can be attached to the aft end of the PDU. In this aircraft the PDU is hard mounted to a pre-aligned mounting frame, rather than an adjustable Mounting Tray i.e. it is already boresighted to the airframe. The drawback to the installation is that the PDU has to be long and narrow which is reflected in the design of the circuit boards within the unit. The High Voltage Power Supply locates on the underside of the PDU and there would be a Gun Camera and an Up-Front Control Panel fitted to customer requirements.

 

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