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Marske XM 1

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Wingspan
  
12 m

Length
  
2.48 m

Marske XM-1 httpsuploadwikimediaorgwikipediaenthumbb

The Marske XM-1 was an American mid-wing, single-seat, experimental tailless glider that was designed and built by Jim Marske in 1957.

Contents

Experimentation with the XM-1 lead 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 though 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 though 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 II

General 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; 122 kn (226 km/h)
  • 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)
  • References

    Marske XM-1 Wikipedia