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HAL-3

From Wikipedia, the free encyclopedia

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.[1] The overall technical characteristics are thought to be similar to the Bendix AN/APS-133/RDR-1F.

Specifications

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  • Range:
    • air-to-ground mode : 240 km
    • air-to-air mode: 15 km
  • Output power: 50 kW
  • Power consumption: 800W
  • Weight: 9999 kg

References

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  1. ^ Zhenhe, Fang; Jun, Zhang; Yi, Wang (July 1996). "The HAL-3 airborne navigation radar". IEEE Transactions on Aerospace and Electronic Systems. 32 (3): 1208–1211. Bibcode:1996ITAES..32.1208F. doi:10.1109/7.532286. Retrieved 2024-03-01.
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