KR 2

On June 1, 1974, the KR-2, a two seat version emerged into the world of experimental aviation with its maiden flight. The prototype KR-2, N4KR, was powered by an 1834cc Revmaster, which is an otherwise stock 1600cc VW with 99mm cylinders. This particular engine was a single ignition version and used a Bendix mag and a Posa carburettor. Revmaster gives the engine a continuous rating of 60 hp at 3000 rpms, which is on the conservative side. Ken Rand, the designer/builder, obtained cruise speeds of 180mph at 3200 rpm and airspeeds of 200mph at higher altitudes. Some aircraft have not been built sufficiently lightweight and became in effect single seaters.

A KR2 fitted with a Jabiru engine (lighter with more power) has flown from the UK to Australia and back with 2 people.

specifications
 
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range
VW 2100
x
14' 6"
x
20' 8"
80 sq. ft.
420 lbs.
480 lbs.
x

900 lbs.
35 gal
1600 miles

performance

takeoff distance, ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling
350 ft.
800 fpm
200 mph
180 mph
900 ft.
15,000 ft.

limiting and recommended speeds

design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed
x
x
52 mph
x

All specifications are based on manufacturer's calculations
Fixed conventional or trigear, or retractable conventional