MMIST CQ-10 SnowGoose
CQ-10 SnowGoose | |
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UAV on a Humvee. | |
Role | Unmanned Aerial Vehicle (UAV) Type of aircraft |
Manufacturer | MMIST |
First flight | April 2001 |
Introduction | January 2005 |
Primary user | USSOCOM |
Number built | CQ-10A: 15 (49 planned) |
The MMIST CQ-10A SnowGoose is a cargo delivery unmanned aerial vehicle that has reached IOC (Initial Operational Capability) with the United States Armed Forces with the delivery of 15 vehicles. The SnowGoose UAV is produced by the Canadian company Mist Mobility Integrated Systems Technology (MMIST). The SnowGoose UAV is an application of MMIST's Sherpa autonomous GPS-guided parafoil delivery system and is intended for pin-point delivery of small cargo items (ammunition, supplies) to special forces. A fully loaded Snowgoose can carry a total of 272 kg (600 lb).[1][2] The SnowGoose was originally designed for leaflet dispensing, but can support a variety of missions with its six modular cargo bays, each of which can carry pods for fuel (trading payload for range), cargo, or electronics (sensor or broadcasting) packages.
The CQ-10A uses a parafoil for lift; the CQ-10B uses an autogyro rotor for lift. The "B" version has twice the range of the "A" version. According to the manufacturer, the CQ-10B can carry 1088 kg (2400 lb) up to 150 km (93 mi) from a central base per day (24 h), placing the loads within 30 m (100 ft) of a predesignated point then performing near-vertical take-offs.[3]
Variants
![](http://upload.wikimedia.org/wikipedia/commons/thumb/2/28/MMIST_CQ-10A_Snow_Goose_%E2%80%9811%E2%80%99_%2826773697244%29.jpg/250px-MMIST_CQ-10A_Snow_Goose_%E2%80%9811%E2%80%99_%2826773697244%29.jpg)
- CQ-10A
- Parafoil lift.
- CQ-10B
- Autogyro rotor lift with increased range. VSTOL.
Operators
Canada
- Canadian Forces - testing 2007
United States
Specifications
- Length 2.90 m (9 ft 6 in)[2]
- Wing Span: 2.1 m (6 ft 8 in)[2]
- Weight max: 635 kg (1400 lb); empty: 270 kg (600 lb)[2]
- Cargo weight max: 272 kg (600 lb) ("A" version)[2] / (227 kg) (500 lb) ("B" version)[3]
- Engine: Rotax 914 piston engine; 81 kW (110 hp)[2]
- Range: 300 km (160 nmi) (34 kg (75 lb) payload)("A" version)[2] / 600 km (320 nmi) ("B" version)[3]
- Endurance: 19 hrs [2]
- Speed: 61 km/h (38 mph)("A" version)[2] / 120 km/h (75 mph ("B" version/ est.)[3]
- Ceiling: >5500 m (18000 ft)[2]
See also
- History of unmanned aerial vehicles
- Unmanned Aerial Vehicle
Related lists
References
- ^ MMIST Inc.
- ^ a b c d e f g h i j Directory of U.S. Military Rockets and Missiles - CQ-10
- ^ a b c d "MMIST Inc". Archived from the original on 2017-07-19. Retrieved 2010-07-18.
External links
- DefenseLink - SnowGoose: UAVs Enter the Airlift Business
- MMIST CQ-10 SnowGoose - Directory of U.S. Military Rockets and Missiles
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(1924-1947)
Controllable bombs | |
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Target control aircraft | |
Aerial target (subscale) | |
Aerial target (full-scale)2 |
(1948-1962)
(1962-present)
Main series | |
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Non-sequential |
- 1 Not assigned
- 2 Not to be confused with the Attack or Amphibious aircraft sequences.
- 3 Assigned to multiple types
- Drones designated in missile sequence