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
|