{| |} 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.
| Attributes | Values |
|---|---|
| rdf:type | |
| rdfs:label |
|
| rdfs:comment |
|
| sameAs | |
| empty weight kg |
|
| dcterms:subject | |
| dbkwik:military/pr...iPageUsesTemplate | |
| ceiling ft |
|
| climb rate ftmin |
|
| met or eng? |
|
| eng1 type |
|
| endurance h |
|
| gross weight kg |
|
| length in |
|
| Type |
|
| eng1 kW |
|
| height m |
|
| Height in |
|
| span m |
|
| climb rate ms |
|
| Manufacturer | |
| max speed kmh |
|
| empty weight lb |
|
| Capacity |
|
| ceiling m |
|
| cruise speed kmh |
|
| length m |
|
| max speed mph |
|
| National Origin |
|
| length ft |
|
| Height ft |
|
| span ft |
|
| cruise speed mph |
|
| gross weight lb |
|
| span in |
|
| Crew |
|
| eng1 hp |
|
| ref |
|
| eng1 number |
|
| abstract |
|