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Melsheimer FM-1

From Wikipedia, the free encyclopedia

FM-1
The FM-1 in its original prototype configuration with the T-tail
General information
TypeGlider
National originUnited States
Designer
StatusProduction completed
Number builtOne
History
Introduction date1968
First flight1968

The Melsheimer FM-1 is an American single-seat, high-wing, FAI Open Class glider that was designed and constructed by Frank Melsheimer.[1][2][3]

Design and development

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The FM-1 was first flown in 1968. The designation indicates the designer's initials.[1][2]

The FM-1 features mixed construction. The aft fuselage and wings are constructed from wood, with the forward fuselage made from welded steel tubing, covered in fibreglass. The wing employs a NACA 4400R airfoil. The aircraft was originally constructed with a T-tail, but this was later changed to a conventional low tail. The cockpit accommodation is one seat in a semi-reclining position.[1][2]

Only one example was completed and registered in the Experimental - Amateur-built category.[1][2][3]

Operational history

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As of May 2011 the FM-1 was still on the Federal Aviation Administration registry.[3]

Specifications (FM-1)

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Data from Sailplane Directory and Soaring[1][2]

General characteristics

  • Crew: one
  • Wingspan: 51 ft 0 in (15.54 m)
  • Wing area: 125 sq ft (11.6 m2)
  • Aspect ratio: 21:1
  • Airfoil: NACA 4400R
  • Empty weight: 500 lb (227 kg)
  • Gross weight: 750 lb (340 kg)

Performance

  • Maximum glide ratio: Estimated 35:1 at 60 mph (97 km/h)
  • Rate of sink: 108 ft/min (0.55 m/s) at 40 mph (64 km/h)
  • Wing loading: 6.0 lb/sq ft (29 kg/m2)

See also

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Related lists

References

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  1. 1 2 3 4 5 Activate Media (2006). "FM-1 Melsheimer". Archived from the original on August 19, 2012. Retrieved May 30, 2011.
  2. 1 2 3 4 5 Said, Bob: 1983 Sailplane Directory, Soaring Magazine, page 48. Soaring Society of America November 1983. USPS 499-920
  3. 1 2 3 Federal Aviation Administration (May 2011). "Make / Model Inquiry Results". Retrieved May 15, 2011.