HAL-3
{{about||the US Navy Helicopter Attack Squadron (Light) 3|HA(L)-3}}
The HAL-3 is an airborne navigation radar developed by the Shanghai Institute of Electron Physics originally for the Y-10 programme. Development started in June 1980 and was completed in February 1985 and it has been extensively tested on the Boeing 707 and Y-7.{{Cite journal |title=The HAL-3 airborne navigation radar |url=https://ieeexplore.ieee.org/document/532286 |access-date=2024-03-01 |journal=IEEE Transactions on Aerospace and Electronic Systems|date=July 1996 |volume=32 |issue=3 |pages=1208–1211 |doi=10.1109/7.532286 |last1=Zhenhe |first1=Fang |last2=Jun |first2=Zhang |last3=Yi |first3=Wang |bibcode=1996ITAES..32.1208F |url-access=subscription }} The overall technical characteristics are thought to be similar to the Bendix AN/APS-133/RDR-1F.
Specifications
- Range:
- air-to-ground mode : 240 km
- air-to-air mode: 15 km
- Output power: 50 kW
- Power consumption: 800W
- Weight: 9999 kg
References
{{Reflist}}
External links
- [https://ieeexplore.ieee.org/stamp/stamp.jsp?arnumber=303760 The HAL-3 radar test set - Aerospace and Electronic Systems, IEEE 1994]