| RJJ-1 Gypsy Hawk | |
|---|---|
 | |
| Jameson Gipsy Hawk at the Rishon LeZion Air and Space Museum | |
| Role | Single seat homebuilt light aircraft |
| National origin | U.S. |
| Designer | Richard J. Jameson |
| First flight | 1972 |
| Number built | 1 |
The Jameson RJJ-1 Gipsy Hawk was a single-engine light aircraft intended to be homebuilt from plans. The prototype was designed and constructed in the U.S. by Richard Jameson in the late 1960s-early 1970s.
The Gypsy Hawk was an all-metal low wing monoplane, constructed throughout from light alloy angle spars and frames under a light alloy skin. The wings and tailplane had constant chord and square tips. There was a fuel tank in the outer panel of each wing. The all-moving tail was set at the extreme rear fuselage and had external mass balances and an anti-servo tab. The fin and rudder were further forward, swept and with a fillet to lead the fin into the strongly sloping upper fuselage. [1]
The fuselage was a light alloy semi-monocoque with a nose-mounted 65 hp (48 kW) Continental A65 flat-four engine driving a fixed pitch, two-blade propeller. The single-seat cockpit placed the pilot over the wing under a two-piece blown canopy. The Gypsy Hawk had a fixed, unfaired tricycle undercarriage. [1]
Construction of the Gypsy Hawk began about 1968 and the first flight was in 1972. [1] [2]
By the end of February 1974 the Gypsy Hawk had logged 200 hours of testing [1] but there is no record of other examples. [2]
By November 2012 the sole example was no longer registered in the United States with the Federal Aviation Administration and may no longer exist. [3]
Data from Jane's All the World's Aircraft 1974-75 [1]
General characteristics
Performance
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