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HTT-40 vs T-25 Universal

HTT-40 vs T-25 Universal at a glance — top speed 450 vs 300 km/h, range 1,000 vs 1,500 km, max takeoff weight 2,800 vs 1,700 kg, built 2 vs 189 units.

HAL HTT-40 military training aircraft side profile drawing
🇮🇳 HTT-40
Neiva T-25 Universal military training aircraft side profile drawing
Specifications
HTT-40 T-25 Universal
Origin country 🇮🇳 India 🇧🇷 Brazil
Category Military Training Aircraft Military Training Aircraft
Manufacturer HAL Neiva
First flight 1 June 2016 29 April 1966
Year introduced 2026 1971
Number produced 2 units 189 units
Average unit price $12.1 million --
Wing area -- m² 17.2 m²
Wingspan 11.0 m 11.0 m
Height -- m 3.0 m
Length -- m 8.6 m
Maximum speed 450 km/h 300 km/h
Operational range 1,000 km 1,500 km
Service ceiling 6,000 m 6,100 m
Max. takeoff weight 2,800 kg 1,700 kg
Empty weight 2,000 kg 1,150 kg
Total thrust 1 x 708 kW 1 x 220 kW
Performance Radar Chart
Change comparison vs

Frequently Asked Questions

Which is faster, the HTT-40 or T-25 Universal?
The HTT-40 is faster with a maximum speed of 450 km/h compared to the T-25 Universal's 300 km/h, a difference of 150 km/h.
Which has longer range, the HTT-40 or T-25 Universal?
The T-25 Universal has a longer range at 1,500 km compared to the HTT-40's 1,000 km.
Which can fly higher, the HTT-40 or T-25 Universal?
The T-25 Universal has a higher service ceiling at 6,100 meters (20,013 ft) compared to the HTT-40's 6,000 meters (19,685 ft).
Which is heavier, the HTT-40 or T-25 Universal?
The HTT-40 has a higher maximum takeoff weight at 2,800 kg compared to the T-25 Universal's 1,700 kg.
Which entered service first, the HTT-40 or T-25 Universal?
The T-25 Universal entered service first in 1971, 55 years before the HTT-40 which entered service in 2026.
Which has been built in greater numbers, the HTT-40 or T-25 Universal?
The T-25 Universal has been produced in greater numbers with 189 units compared to 2 units of the HTT-40.