- Aircraft Overview
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HAL ALH Dhruv Mark I
The Advanced Light Helicopter Dhruv Mark I configuration included mechanical gauges in the (conventional) cockpit, the TM 333-2B2 engine, an Anti-Resonance Vibration Isolation System (ARIS) and Frahm dampers (developed by LORD Corporation). The fuel capacity, useful load and under slung load are 1055 kg, 2490 kg, and 1500 kg, respectively. Passenger capacity is 12-14 plus the crew.
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HAL ALH Dhruv Mark I
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HAL ALH Dhruv Mark I
This content is reserved for AHS members. If you are a current member, please use the Member Login link at the top of the page.
If you are not a member of AHS, why not join today? Be sure to also check out the many benefits enjoyed by AHS members.
HAL ALH Dhruv Mark I
This content is reserved for AHS members. If you are a current member, please use the Member Login link at the top of the page.
If you are not a member of AHS, why not join today? Be sure to also check out the many benefits enjoyed by AHS members.
HAL ALH Dhruv Mark I
This content is reserved for AHS members. If you are a current member, please use the Member Login link at the top of the page.
If you are not a member of AHS, why not join today? Be sure to also check out the many benefits enjoyed by AHS members.
HAL ALH Dhruv Mark I
This content is reserved for AHS members. If you are a current member, please use the Member Login link at the top of the page.
If you are not a member of AHS, why not join today? Be sure to also check out the many benefits enjoyed by AHS members.
HAL ALH Dhruv Mark I
- Forum Proceedings (0)
- Vertiflite articles (0)
- AHS website (2)
- Journal articles (?)
- NASA NTRS (?)
- USPTO Patents (?)
- Google Books (?)
Forum Proceedings related to the HAL ALH Dhruv Mark I
We were unable to find any Forum Proceedings for this aircraft.
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