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Pakistan Male UAV official Specs

GiG

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Good optics, good munitions, and SATCOM and this thing will be a great UCAV.

Interesting, AESA for UAV? In theory you could install BVR missiles for engaging of enemy aircraft but the performance won't be as good as what can be achieved with fighter jets.


"AESA radar development is also under progress in order to achieve independency and life cycle support and later on integrate the Radar in the target platforms like JF-17, MALE UAV and other systems."
 
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1,596 kg MTOW. Nice!

@JamD It looks like PAC found a higher-rated engine versus the Anka-A and CH-4.

Basically,

NESCOM: "we got landing gear-"

AvRID: "we designed the largest Pakistani plane."

NESCOM: "...where do you live, sorry?"

In terms of MTOW, where would this place the upcoming Pakistani drone, among global competitors?
 
1,596 kg MTOW. Nice!

@JamD It looks like PAC found a higher-rated engine versus the Anka-A and CH-4.

Basically,

NESCOM: "we got landing gear-"

AvRID: "we designed the largest Pakistani plane."

NESCOM: "...where do you live, sorry?"
Is this drone better than predator?
 
If PAC has the chance to buy PD170 or PD222, which he will, I laugh if they doesn't use them. Your friendly country has an engine that give 100 HP at 30k feet and can reach a maximum altitude of 40k, and you limit yourself to 25000 feet.
Let the Indian air defenses in Keshmir consider what can and cannot use.
 
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1,596 kg MTOW. Nice!

@JamD It looks like PAC found a higher-rated engine versus the Anka-A and CH-4.

Basically,

NESCOM: "we got landing gear-"

AvRID: "we designed the largest Pakistani plane."

NESCOM: "...where do you live, sorry?"


I would like to see some specs issued by PAC, since these seem like design specifications/goals and not the actual specifications, but let's take these at face value.

Firstly, the height has to be a typo. 3ft makes no sense. We saw the prototype and we are 200% sure it wasn't that small.

The engine. Interesting how it has exactly the same bhp as the Lycoming engine on the Mushaak. Makes sense to have a common engine.

Some rough math:
MTOW = 3520 lb
Armament = 771 lb
Empty = 1980 lb

Fuel(?) = 3520-771-1980 = 769 lb
Fuel Fraction (?) = 769/(3520-771) = 0.28 (for comparison MQ-1 has a fuel fraction of 0.45 or something, which points to lightweight structure)

Fuel Volume(?) = 490 L
Lycoming Endurance = 30-34 L / hr
Endurance of UAV = 14.4 - 16 hr

Decent, but not crazy. Endurance would be very similar to Shahpar II. Payload much bigger.
 
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