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JUSTAS

Background  —  Canadian Forces  JUSTAS  UAV —  IAI Malat Heron

Israeli UAV family trees are complex and this, along with overlapped DND UAV programs, causes some confusion. The UAVs leased  for CF use in Afghanistan through MacDonald Dettwiler are  IAI Malat Heron 1s. The 'air vehicle' put  forward  for DND's JUSTAS program by MacDonald Dettwiler and IAI is the larger Heron TP. To confuse matters further, a UAV closely related  to the Heron 1 was loaned to DND for the 2003 PLIX trials off  Tofino. This UAV was designated  CU-160 Eagle-1 by the CF.

The leased UAVs in Afghanistan [1] and CU-160 Eagle-1 are powered by piston engines – the same Rotax 914 that powered the earlier Predator A and rival Hermes 900. A small turbo- charged,  4-stroke engine, the Rotax 914 is fuel efficient but somewhat lacking in power. That makes a Heron 1 ideal  for long-range missions with light payloads. However, JUSTAS was changed to include weapon carrying, requiring more power.

Heron TP – also called Heron 2 [2] – is a substantially enlarged development of  the Heron 1 (about half-again larger) but a PT6 turboprop gives the Heron TP a greater all-around performance including a longer endurance, more altitude, and a payload  four times bigger.[3] But, this performance comes at a cost compared with the Heron TP's thiftier predecessor. The take-off weight of a turboprop Heron TP is four times that of  the Heron 1. Still, all the extra power is needed to meet the requirements of  JUSTAS. Although whether IAI gains any points by using a Canadian [4] turboprop remains to be seen.

The IAI Malat Heron family also has 2 export variants – the piston-engined Eagle-1 and the turboprop-powered Eagle-2  (developed with EADS ). Eagle variants  differ in detail from their Heron equivalents (in the wing span particularly). While the UAV for Afghanistan provided through MacDonald Dettwiler will almost certainly be a standard Heron 1, it is possible that an IAI submission for JUSTAS might combine the features of  a  standard Heron TP with the desirable elements from the Eagle series. [5]

  Specifications:   IAI  Malat Heron 1  (Mahatz / ShovalUAV
  Performance:   Maximum altitude: 30,000 feet  (9,144 m)  [6]
  Endurance:   40 hours, range: BLOS (beyond-line-of-sight)
  Powerplant:
 
  1 x 115 hp (86 kW)  Rotax 914  turbo  4-stroke
  4-cyl. driving a 2 m diameter, 2-blade propeller
  Dimensions:   Length overall: 8.50 m, wing span: 16.60 m [7]
  Weights:   MTOW: 1,150 kg,  maximum payload: 250 kg
  Specifications:   IAI  Malat Heron TP (Heron 2 / EitanUAV
  Performance:   Maximum altitude: 45,000 feet  (13,716 m)  [8]
  Endurance:   36 hours, range: BLOS (beyond-line-of-sight)
  Powerplant:
 
  1,200 hp (895 kW) P&WC PT6A-67 turboprop
  driving a 2.8 m diameter, 4-blade propeller
  Dimensions:   Length overall: 14.0 m, wing span: 26.0 m
  Weights:   MTOW: 4,650 kg,  typical payload: 1,000 kg

[1]  DND established a precedent in designating leased UAVs (eg: CU-163 Altairs).  It would be logical  that leased Herons are CU-160As.
[2] The naming gets even more confused. In Israeli service, a Heron TP is called Eitan or Mahatz 2. Heron 1 is called Mahatz 1 or  Shoval.
[3]  It has been questioned whether Heron 2s can carry weapons. It seems exceedingly unlikely that IAI would design a UAV which could not be armed.  In any case, a stiffer twin-boomed layout would make mounting weapons even simpler than for the competing Predator Bs.
[4] The PT6A-67 is made by Pratt & Whitney Canada of  Longueuil, Quebec.  The Predator B uses the US-made Garrett TP 331 turboprop.
[5] It also remains to be seen whether MacDonald Dettwiler/IAI's willingness to participate in Project Noctua – the leased and contractor- maintained Heron 1s supporting Canadian troops in Afghanistan – will have any influence over DND's decision over JUSTAS purchases.
[6] CU-160 Eagle-1 altitude is 25,000-to-32,000 feet. Endurance is 30 hours with loiter times of 12 hours at 1,018 km and 7 hours at 1,481 km.
[7] Dimensions of  the CU-160 Eagle-1 variant differ slightly, being shorter in span (16.30 m)  but  greater in fuselage/boom length (8.94 m).
[8] This is the target altitude. On 10 Sept 2008, the Heron TP established a new record altitude by flying at 40000 ft  for an extended period.