Rensselaer RP-3

Source: Wikipedia, the free encyclopedia.

RP-3
Role Glider
National origin United States
Manufacturer Rensselaer Polytechnic Institute
Designer Brian E. Thompson
Introduction 1998
Status Sole example on display in the New York State Museum
Number built one

The Rensselaer RP-3 (for Rensselaer Polytechnic design 3) is an American

mid-wing, T-tailed single-seat, glider that was designed by Brian E. Thompson and produced by the Rensselaer Polytechnic Institute of Troy, New York.[1][2] It first flew in 1998.[3]

Design and development

The RP-3 was the third aircraft design in Rensselaer's Composite Aircraft Program and was completed in 1998.[1][2]

The aircraft is of composite construction. Its 54 ft (16.5 m) span wing employs a Wortmann FX-67-K170/17

glide ratio.[1][4]

Only one RP-3 was built and it was registered with the Federal Aviation Administration in the Experimental - Amateur-built category.[1]

Aircraft on display

Specifications (RP-3)

Data from Sailplane Directory[1]

General characteristics

  • Crew: one
  • Wingspan: 54 ft 0 in (16.46 m)
  • Wing area: 179.76 sq ft (16.700 m2)
  • Aspect ratio: 17:1
  • Airfoil: Wortmann FX-67-K170/17
  • Empty weight: 650 lb (295 kg)
  • Gross weight: 1,000 lb (454 kg)

Performance

  • Maximum glide ratio: 32:1 at 51 mph (82 km/h)
  • Rate of sink: 136 ft/min (0.69 m/s) at 45 mph (72 km/h)
  • Wing loading: 5.56 lb/sq ft (27.1 kg/m2)

See also

Related lists

References

  1. ^ a b c d e Activate Media (2006). "Rensselaer RP-3". Archived from the original on September 2, 2012. Retrieved August 24, 2011.
  2. ^ a b Federal Aviation Administration (August 2011). "Make / Model Inquiry Results". Retrieved August 24, 2011.
  3. ^ "J2mcL Planeurs - Fiche planeur n°". www.j2mcl-planeurs.net. Retrieved May 21, 2022.
  4. ^ Lednicer, David (2010). "The Incomplete Guide to Airfoil Usage". Retrieved August 1, 2011.
  5. ^ Berek, Daniel L. (May 2011). "Aircraft N397RP Photo". Retrieved August 24, 2011.

External links