For Northrop, under a US Air Force contract, DSI designed, built and flight tested an electrically-propelled mini-RPV named Scout. Development continued by DSI as a company-funded programme, with a new engine and autopilot. Experimental flights were continuing in 1978, the Scout having recently flown with two different power plants. One was an electric motor powered by lithium batteries, using a small petrol engine for launch only; the other was a low-cost 3-7 kW (5 hp) two-stroke engine, installed for harassment RPV development.
Airframe: Sweptback shoulder-wing monoplane, with servo-actuated trailing-edge elevons and sweptback endplate fin at each wingtip. Wings, elevons and fins have Kevlar skins, with partial urethane foam support. Tapered body, of super-elliptical cross-section, built of bulkheads and Kevlar skin and having detachable nose-cap. Non-retractable tricycle landing gear.
Power Plant: See introductory copy.
Launch and Recovery: Conventional wheeled T-O and landing standard.
Guidance and Control: As for Sky Eye.
Equipment: DSl-PSA-WL-OI stability augmentation autopilot. Eight telemetry channels to monitor speed, altitude, autopilot functions and onboard sensors.
Dimensions, external:
Wing span 2-715 m (8 ft 10-92 in)
Wing area, gross 1-38 m^ (14-86 sq ft)
Length overall 0-91 m (3 ft in)
Height overall 0-20 m (8-04 in)
Weights:
Weight empty, equipped 15-4 kg (34 lb)
Max T-O weight 25 kg (55 lb)
Performance (at max T-O weight):
Max level speed 60 knots (111 km/h; 69 mph)
Stalling speed 32-5 knots (60 km/h; 37 mph)
Max rate of climb at S/L 91 m (300 ft)/min
E-SYSTEMS E-75, E-90, E-130, E-150, E-175, E-200, E-260 and E-310
The first in Melpar’s developing family of single-tailboom minis was the E-75, which in 1977-78 became a candidate in the US Air Force’s LCEHV (low cost expendable harassment vehicle) programme.
Three photos of the MBB Locust, which I had to restore as the copies were stained and cut in places (see fourth image). They were found in the Ryan Aeronautical Archives.
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