The Marske XM-1 was an American mid-wing, single-seat, experimental tailless glider that was designed and built by Jim Marske in 1957. Experimentation with the XM-1 led to the final configuration of the later Marske Pioneer.
Design and development The first of Marske's flying wings was the XM-1, a design inspired by the flying wing designs of Charles Fauvel and Al Backstrom. He built the XM-1 when he was 19 years old. The aircraft went through several versions, each a modification of the same basic airframe as Marske experimented with configurations. The aircraft started off with fins on the wing tips and was later converted to a single fin at the rear of the short fuselage in its "XM-1D" configuration. The XM-1 was built with a welded steel tube fuselage covered in fiberglass. The 40 ft (12.2 m) wing was fabricated from wood and covered with doped aircraft fabric. The wing employed a 14% Fauvel airfoil. The landing gear was a fixed monowheel. Only one XM-1 was built. It was registered with the US Federal Aviation Administration in the Experimental - Amateur-built category.
Operational history The XM-1 was described by Soaring Magazine as "easy to fly". The aircraft was stall and spin proof. Marske sold the aircraft and it went through a series of owners. The XM-1 was later removed from the FAA register and likely no longer exists.
Variants XM-1-A Initial configuration with wing tip fins and rudders. XM-1-B with minor improvements over the XM-1-A XM-1-C Modified with a central fin only. XM-1D Final configuration with a central fin and rudder.
Specifications (XM-1B) Data from The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde Volume IIGeneral characteristics Crew: one Length: 8 ft 2 in (2.48 m) Wingspan: 38 ft 1 in (11.6 m) Height: 3 ft 10 in (1.16 m) at cockpit Wing area: 160 sq ft (15 m2) Aspect ratio: 9 Airfoil: 14% Fauvel Empty weight: 311 lb (141 kg) Gross weight: 551 lb (250 kg) Performance
Never exceed speed: 140 mph (226 km/h, 122 kn) Aerotow speed: 104.5 mph (90.8 kn; 168.2 km/h) Winch launch speed: 105 km/h (65.2 mph; 56.7 kn) g limits: +4 -3 at 65.25 mph (56.7 kn; 105.0 km/h) Maximum glide ratio: 24:1 at 51 mph (44.3 kn; 82.1 km/h) Rate of sink: 175 ft/min (0.89 m/s) at 39.8 mph (34.6 kn; 64.1 km/h) Wing loading: 3.4 lb/sq ft (16.7 kg/m2)
See also
Related lists
List of gliders
References
External links Official website


