FORCETALLY
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Measured figures
Configuration
| Specification | Sukhoi S-70 Okhotnik-B | Tengden TB-001 |
|---|---|---|
| Crew | None[source] | None[source] |
| Type | Unmanned combat aerial vehicle Loyal wingman drone (future)[source] | Medium-altitude long-endurance unmanned aerial vehicle[source] |
| National origin | Russia[source] | China[source] |
| Manufacturer | Novosibirsk Aircraft Production Association Plant[source] |
Empty; Sukhoi S-70 · not confirmed
Single sourceMaximum take-off; Sukhoi S-70 · Max takeoff weight
Single source10,000 to 20,000 kg (22,046 to 44,092 lb) (not confirmed)[source]
25,000 kg (55,116 lb)[source]
Maximum take-off; Max takeoff weight
Single source2,800 kg (6,173 lb)[source]
Maximum; Sukhoi S-70 · 0.82 Mach
Single source1,000 km/h (620 mph, 540 kn) 0.82 Mach[source]
Sukhoi S-70 · Combat range
Single source3,000 km (1,900 mi, 1,600 nmi)[source]
Service ceiling
Single source8,000 m (26,000 ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Sichuan Tengden[source]
| Designer | Sukhoi Mikoyan[source] | Koen Lee Choi[source] |
|---|
| Status | In development[source] | — |
|---|
| Primary user | Russian Aerospace Forces[source] | People's Liberation Army[source] |
|---|
| Number built | — |
|---|
| Manufactured | 2019–present[source] | — |
|---|
| Introduction date | 2024[source] | — |
|---|
| First flight | 3 August 2019[source] | — |
|---|
| Developed from | Mikoyan Skat Sukhoi Su-57[source] | — |
|---|
| Powerplant | 1 × AL-41F derivative[source] | — |
|---|
| Capacity | — | 1,200 kg (2,646 lb) payload[source] |
|---|
| Hardpoints | — | 4 hardpoints[source] |
|---|
| Role | — | medium-altitude long-endurance (MALE) unmanned combat aerial vehicle (UCAV)[source] |
|---|
| Source measurement | — | TB-001A: Developed from the original TB-001. Upgraded with an additional engine on the tail. Maximum takeoff weight increased from 2,800 kilograms of the original TB-001 to 3,200 kilograms (7,100 lb), payload from 1,200 kilograms to 1,500 kilograms (3,300 lb), and flight ceiling from 8,000 metres to 9,500 metres (9,000 m sustained). Takeoff distance is shortened to 500 metres and has maximum rate of climb of over 10 metres per second. The maximum flight endurance is 35 hours, the same as TB-001.[source]Tengden TB-001 · Variants; only the objects and conditions stated in this passage Capacity: 1,200 kg (2,646 lb) payload[source]Tengden TB-001 · Specifications; only the objects and conditions stated in this passage Length: 10 m (32 ft 10 in)[source]Tengden TB-001 · Specifications; only the objects and conditions stated in this passage Wingspan: 20 m (65 ft 7 in)[source]Tengden TB-001 · Specifications; only the objects and conditions stated in this passage Height: 3.3 m (10 ft 10 in)[source]Tengden TB-001 · Specifications; only the objects and conditions stated in this passage Max takeoff weight: 2,800 kg (6,173 lb)[source]Tengden TB-001 · Specifications; only the objects and conditions stated in this passage Range: 6,000 km (3,700 mi, 3,200 nmi)[source]Tengden TB-001 · Specifications; only the objects and conditions stated in this passage Endurance: 35 hours with 1,000 kg payload[source]Tengden TB-001 · Specifications; only the objects and conditions stated in this passage Service ceiling: 8,000 m (26,000 ft)[source]Tengden TB-001 · Specifications; only the objects and conditions stated in this passage 250 kg laser-guided bomb, FT -7 glide bomb, FT-9 guided bomb[source]Tengden TB-001 · Specifications; only the objects and conditions stated in this passage 280 km communication range with line of sight ground command post, 3,000 km communication range with satellite communication data links[source]Tengden TB-001 · Specifications; only the objects and conditions stated in this passage |
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