The V-Star was designed as a low-cost, economical and easy to fly design, with a light wing loading and short runway requirements. It features a strut-braced biplane layout, with cabane struts, interplane struts and flying wires, a single-seat open cockpit, fixed conventional landing gear with wheel pants and a single engine in tractor configuration.
The aircraft fuselage is made from welded 4130 steel tubing. Its 231NaN1 span wings are made from spruce and plywood, with the whole aircraft covered with doped aircraft fabric. The wings employ a Clark YH airfoil and have a total area of 141square feet. The engine used is the 650NaN0 Continental A65 or other similar powerplants.[2]
The V-Star has a typical empty weight of 700lb and a gross weight of 1000lb, giving a useful load of 300lb. With full fuel of the payload for the pilot and baggage is 210lb.
The standard day, sea level, no wind, take off with a 650NaN0 engine is 4000NaN0 and the landing roll is 6000NaN0.
The designer estimates the construction time from the kit that was available in the 1990s as 1800 hours.
By 1998 the company reported that 65 aircraft were completed and flying.
In March 2014, 13 examples were registered in the United States with the Federal Aviation Administration, although a total of 24 had been registered at one time. In Canada in March 2014 there were two registered with Transport Canada and in the United Kingdom a further two were registered with the CAA.[3] [4] [5]