Robertson Skylark SRX-1 explained

The Robertson Skylark SRX-1 is a five place high performance STOL aircraft designed in the 1950s. It was intended to be operated out of 1200NaN0 landing strips with 1500NaN0 cruise speeds.[1]

Design

The aircraft was designed by James L. Robertson, son of William B. Robertson, Robertson Aircraft Corporation founder at the age of 27. The aircraft is designed to be stall-proof and spin-proof and is capable of a 250NaN0 minimum flight speed. It was also the first light aircraft in America to be designed to accommodate a turboprop engine.[2]

The Skylark is all metal, with a steel tube internal structure. It incorporates shrouds, flaps, spoilerons, turbulator control, stabilators, elevators, and spinner duct cooling.[3]

Operational history

Test flights were performed by aerobatic pilot Marion Cole. He featured the aircraft as part of his Cole Brothers airshows. The aircraft is able to take off in 100 feet.

External links

Notes and References

  1. Flying Magazine. July 1954. 37.
  2. Experimenter. Project Skylark. April 1955.
  3. Book: Survey of research projects in the field of aviation safety, Issue 6 Cornell University. Daniel and Florence Guggenheim Aviation Safety Center.