India has spent years presenting scale models, artistic concepts and future requirements as evidence of an approaching unmanned revolution. Pakistan’s newer disclosures disturb that comfortable narrative because Islamabad is no longer showing one isolated tactical drone; its defence ecosystem is beginning to reveal a layered family spanning long-range piston-powered strike aircraft, arrow-delta loitering munitions, high-speed jet-powered anti-radiation systems, swarming weapons and counter-drone integration.
But Pakistan must resist its own temptation to turn brochures into battalions.
The evidence supports a strong conclusion, though not the exaggerated one circulating across social media: Pakistan presently appears to be pursuing a more operationally focused and diversified one-way-attack-drone portfolio, while India retains greater industrial scale, a broader conventional UAV programme and more procurement depth. Pakistan’s advantage is visible in the clarity of its emerging mission architecture; India’s advantage lies in resources, institutional breadth and its ability to place substantial orders. Neither country has publicly proven every capability being claimed.
That distinction matters because a model can demonstrate aerodynamic intent, a displayed airframe can demonstrate fabrication, and a flight-test announcement can demonstrate development activity—but only repeated trials, serial production, unit induction and operational employment demonstrate military capability.
What Pakistan Has Actually Revealed
Heavy Industries Taxila presented the D-248 and S-369 during the 2026 Indus Robotics and Autonomous Systems Expo. Photographs of their display boards provide unusually specific performance figures, while independent defence reporting records the same published values.
The D-248 is described as a tailless delta-wing loitering munition with a 3.3-metre wingspan, approximately 240-kilogram maximum take-off weight, a 30–50-kilogram payload, 185 km/h cruising speed, 225 km/h maximum speed, a ceiling of 4,500 metres and 12–14 hours of endurance. Its most consequential advertised figure is an operational range of 2,200–3,000 kilometres. The S-369 follows an arrow-delta arrangement and is advertised with a four-metre wingspan, 215–225-kilogram maximum take-off weight, the same 30–50-kilogram payload class, 160–180 km/h cruising speed, 220 km/h maximum speed and a 1,500–2,000-kilometre operating range. These figures are corroborated by the display material and summarised by Quwa’s reporting on the HIT systems.
| Pakistani system | Publicly presented role | Published performance | Evidence level |
|---|---|---|---|
| D-248 | Long-range delta-wing loitering munition | 2,200–3,000 km range; 30–50 kg payload; 12–14 hours; 225 km/h maximum speed | Manufacturer exhibition specifications; operational performance not independently verified |
| S-369 | Arrow-delta long-range loitering munition | 1,500–2,000 km range; 30–50 kg payload; 160–180 km/h cruise; up to 220 km/h | Manufacturer exhibition specifications; operational performance not independently verified |
| Nimbus2K | Jet-powered anti-radiation strike system | 75 kg MTOW; up to 650 km/h cruise; 10 kg payload; 10,000-metre ceiling; up to 150 minutes | Company specifications accompanied by reported flight-testing activity |
| HiMark-25 TJ | Turbojet loitering munition for swarm, SEAD and DEAD missions | 70 kg MTOW; 25 kg warhead class; 240 km/h cruise; 320 km/h dash; 250 km range | Company specifications and reported flight-testing material |
| POF “Killer Drone” | Delta-wing one-way attack system | No authoritative public performance sheet identified | Physical display reportedly seen; relationship with D-248 remains publicly unresolved |
The specification table is not a certificate of combat performance. It is evidence of what Pakistani manufacturers say they are designing, testing or offering. Nevertheless, that evidence cannot honestly be dismissed as “Chinese toys” merely because social-media accounts dislike Pakistan. Defence technology does not become imaginary simply because its manufacturer is Pakistani, just as it does not become operational merely because a brochure prints an impressive range.
Why Nimbus2K and HiMark-25 Matter More Than Another Long-Range Drone
The most interesting development may not be the much-publicised 3,000-kilometre D-248. It may be Woot Tech’s attempt to build complementary jet-powered systems for suppressing and destroying enemy air defences.
The company describes Nimbus2K as a jet-propelled anti-radiation cruise missile intended for radars and command-and-control centres. Its published sheet gives it a 75-kilogram maximum take-off weight, three-metre wingspan, 2.5-metre fuselage, up to 650 km/h cruising speed, a claimed 100-kilometre communications range, up to 150 minutes of endurance, a ten-kilogram payload and a service ceiling of 10,000 metres.
HiMark-25 TJ occupies a different envelope. Its presented specifications include a three-metre length, 2.5-metre wingspan, 70-kilogram maximum take-off weight, 240 km/h cruising speed, 320 km/h dash speed, 250-kilometre range, 60-minute endurance and 4,500-metre ceiling. The accompanying material emphasises vehicle-mounted rail launchers, rocket-assisted take-off, swarm employment and mission configurations including anti-radiation and bunker-penetrating warheads.
That combination reveals the logic. A slow, long-range delta-wing weapon can pressure fixed infrastructure and force defenders to expend interceptors. A smaller jet-powered weapon can pursue emitting radars or time-sensitive nodes. Swarms and decoys can complicate classification. Electronic warfare, reconnaissance and conventional aviation can exploit whatever gaps emerge.
This is the architecture of suppression of enemy air defences, or SEAD, followed by destruction of enemy air defences, or DEAD. It does not mean Pakistan has publicly demonstrated a mature, networked swarm capable of dismantling any chosen air-defence grid. It means Pakistani industry is visibly working toward the correct mission combination—and that is strategically more meaningful than boasting about a single drone’s maximum brochure range.
India’s HALE Ambition Is Real—but the Propulsion Gap Is Also Real
India should not be caricatured as having no drone industry. It has TAPAS, Archer-NG, the Ghatak-associated technology demonstrator, Nagastra loitering munitions, private-sector systems and substantial institutional capacity distributed among the Defence Research and Development Organisation, Aeronautical Development Establishment, Hindustan Aeronautics Limited and private manufacturers.
Archer-NG has reportedly entered flight development, while the Indian Army has received hundreds of Nagastra-1 systems. India is therefore not standing still, and any Pakistani analysis that ignores its procurement scale would become the mirror image of the propaganda it criticises.
The newly circulated Indian HALE concept, however, remains exactly that: a concept representing a desired high-altitude, long-endurance combat aircraft. Reports associate it with a growing all-up weight potentially reaching roughly 6.7–8 tonnes, turboprop propulsion and possible carriage of weapons including the Astra beyond-visual-range air-to-air missile. Yet even Bharat Dynamics’ official Astra description confirms the missile’s own status and characteristics—not its integration with an operational Indian HALE drone.
| Indian programme | Current significance | Principal limitation |
|---|---|---|
| TAPAS-BH-201 | Important indigenous MALE development and technology base | Did not cleanly mature into the originally expected service outcome |
| Archer-NG | More focused armed MALE successor with reported flight activity | Still undergoing development and validation |
| Proposed ADE HALE UAV | Potentially large turboprop ISR/strike platform with substantial payload growth | Suitable indigenous 900–1,500 shp-class turboprop and full platform validation remain central challenges |
| Nagastra-1 | Evidence that India can procure locally produced tactical loitering munitions in quantity | Represents a shorter-range tactical class, not strategic deep strike |
| Ghatak/SWiFT path | Supports stealthy unmanned combat-aircraft research | Technology-demonstrator progress is not the same as fielded UCAV capability |
The engine problem is not a minor procurement detail. A HALE aircraft expected to operate near 40,000 feet, carry sensors and weapons, survive hot-and-high conditions and retain acceptable take-off performance needs a propulsion system designed around the mission. Suggestions that India convert an Ardiden/Shakti or SAFHAL Aneto-derived turboshaft core into a 1,200–1,500 kW turboprop are technically plausible as an industrial pathway, but a turboprop is not created simply by attaching a propeller to a helicopter engine. Reduction gearing, propeller matching, thermal management, altitude derating, vibration, control software, inlet design, reliability and certification all become programme-defining work.
India’s model may therefore represent a serious future requirement, but it does not yet prove that an eight-tonne indigenous HALE aircraft is ready to fly at 40,000 feet carrying Astra missiles. The recurring frustration expressed even by Indian defence followers—“another project on paper” and “should have been done a decade back”—reflects a genuine gap between India’s conceptual ambition and programme delivery.
