Silver Arrow Micro-V
| Micro-V, Mini-V | |
|---|---|
| Role | Reconnaissance UAV |
| National origin | Israel |
| Manufacturer | Elbit Systems |
| First flight | 1989 |
|
| |
The Silver Arrow Mini-V (originally named the Micro-V) is a small reconnaissance UAV developed in Israel in the 1990s.
It is powered by twin 3 kW (4 horsepower) piston engines, one in a nacelle on each wing driving a pusher propeller. It has no landing gear. The Micro-V appears to be too small to carry a full sensor turret, carrying a miniaturized imager in a transparent section built into the middle of its fuselage.
Specifications
Data from Unmanned Aerial Directory: Part 1[1]
General characteristics
- Crew: None
- Capacity: 8 kg (18 lb) payload
- Length: 2.87 m (9 ft 5 in)
- Wingspan: 3.60 m (11 ft 9¾ in)
- Height: 0.57 m (1 ft 10½ in)
- Empty weight: 27 kg (60 lb)
- Gross weight: 45.5 kg (100 lb)
- Powerplant: 2 × piston engines, 3 kW (4 hp) each each
Performance
- Maximum speed: 204 km/h (127 mph)
- Cruising speed: 93 km/h (58 mph)
- Endurance: 5 hours
- Service ceiling: 4,600 m (15,000 ft)
- Rate of climb: 5.6 m/s (1,100 ft/min)
References
- ↑ Munson Air International July 1996, p. 46.
- Munson, Kenneth. "Unmanned Aerial Vehicles Directory: Part 1". Air International, July 1997, Vol 53 No 1. pp. 40–46.
- Manufacturer's website
- Jane's Unmanned Aerial Vehicles and Targets
This article contains material that originally came from the web article Unmanned Aerial Vehicles by Greg Goebel, which exists in the Public Domain.
Aircraft produced by Elbit Systems | ||
|---|---|---|
| UAVs |
|  |
This article is issued from Wikipedia - version of the 7/7/2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.