| MODEL/DESIGNATION | LENGTH (FT./M) | SPAN (FT./M) | GROSS WEIGHT (LB./KG) | POWERPLANT (NO./TYPE) | POWER/THRUST | PAYLOAD, LB./KG (WT./TYPE) | SPEED (KT./KM/H) | ENDURANCE | MAX. ALTITUDE (FT./M) |
| AAI Corp. | |||||||||
| RQ-7Bv2 Shadow | 11.8/3.596 | 20.4/6.217 | 467/211.8 | 1 × UEL AR741 rotary | 38 hp/28.3 kW | 45-80/20.4-36.2 (EO/IR/LD) | 90-110/ 166-203 | 9 hr. | 15,000/4,572 |
| AeroVironment Inc. | |||||||||
| RQ-11B Raven | 3/0.914 | 4.5/1.371 | 4.2/1.9 | 1 × electric | 200 W | 6.5 oz./184.2 gram (EO/IR) | 17-44/31-81 | 60-90 min. | 500/152.4 |
| RQ-20A Puma AE | 4.6/1.402 | 9.2/2.804 | 13/5.8 | 1 × electric | 600 W | EO/IR | 20-45/37-83 | 2 hr. | 500/152.4 |
| Elbit Systems | |||||||||
| Hermes 450 | 20/6.096 | 34.5/10.515 | 1,200/544.3 | 1 × UEL AR801 rotary | 60 hp/44.7 kW | 400/181.4 (EO/IR/LD) | 70-95/129-175 | 17 hr. | 18,000/5,486.4 |
| General Atomics Aeronautical Systems | |||||||||
| MQ-1C Gray Eagle | 28/8.534 | 56/17.068 | 3,200/1,451.5 | 1 × Thielert Centurion 2.0 HFE | 135 hp/100.6 kW | 1,075/487.6 internal/external | 167/309 | 25 hr. | 29,000/8,839.2 |
| MQ-9 Reaper | 36/10.972 | 66/20.116 | 10,500/4,762.7 | 1 × Honeywell TPE331-10 | 900 shp/671.1 kW | 3,850/1,746.3 internal/external | 240/444 | 27 hr.+ | 50,000/15,240 |
| Insitu | |||||||||
| RQ-21A Blackjack | 7.2/2.194 | 16/4.876 | 135/61.2 | 1 × NWUAV gas/HFE | 8 hp/5.9 kW | 37.5/17.0 (EO/IR/LRF) | 55-80+/ 101-148+ | 24 hr. | 15,000+/4,572+ |
| ScanEagle 2 | 5.6/1.706 | 10.2/3.108 | 51.8/23.4 | 1 × N20 (gas), N21 (HFE) | 2.7 hp/2.0 kW | 7.7/3.4 (EO/IR+) | 50-80/92-148 | 16 hr.+ | 19,500/5,943.6 |
| Israel Aerospace Industries | |||||||||
| Heron TP | 45.9/13.990 | 85.3/25.999 | 10,230/4,640.2 | 1 × P&WC PT6A | 1,200 shp/894.8 kW | 4,400/1,995.8 (EO/IR, SAR, Elint, comm) | 242/448 | 36 hr. | 45,000/13,716 |
| Super Heron HF | – | 55.8/17.007 | 3,200/1,451.5 | 1 × HFE | 200 hp+/149.1+ kW | 990/449.0 (EO/IR, SAR, Elint, comm) | 60-150+/ 111-277+ | up to 45 hr. | 30,000+/9,144 |
| Lockheed Martin | |||||||||
| Fury 1500 | – | 14.3/4.358 | 300+/136.0+ | 1 × HFE | – | 75-125/34.0-56.6 (ISR + EW) | 65-95/120-175 | 15 hr.+ | 15,000/4,572 |
| Northrop Grumman | |||||||||
| MQ-4C Triton | 47.6/14.508 | 130.9/39.898 | 32,250/14,628.4 | 1 × R-R AE3007H | 9,500 lb./42.25 kN | 3,200/1,451.5 internal 2,400/1,088.6 external | 357/661 | 24 hr. | 56,500/17,221.2 |
| MQ-8C Fire Scout | 41.4/12.618 | 35/10.668 (rotor diameter) | 6,000/2,721.5 | 1 × R-R M250-C47E | 700 shp/521.9 kW | 1,000/453.5 internal 2,600/1,179.3 sling load | 140/259 | 12 hr. | 17,000/5,181.6 |
| Piaggio Aero | |||||||||
| P.1HH HammerHead | 47.3/14.417 | 51.2/15.605 | 13,500/6,123.5 | 2 × P&WC PT6A-66B | 850 shp/633.8 kW each | 500/226.7 (EO/IR, SAR) | 395/731 | 16 hr. | 45,000/13,716 |
| Turkish Aerospace Industries | |||||||||
| Anka | 26.2/7.985 | 56.8/17.312 | 3,530/1,601.1 | 1 × HFE | 155 hp/115.5 kW | 440/199.5 (EO/IR/LD, SAR) | 110/203 | 24 hr. | 30,000/9,144 |