Comment:
The HP-14 was developed from the HP-13 which was
essentially a HP-11 fuselage with the Wortmann
airfoil used on the HP-12, with extended span.
That wing was later mated to an improved fuselage
to become the HP-14. The ヨ14 used lower wing
loading and reduced aspect ratio in an attempt to
maximize performance in weak conditions. More
than 40 of all versions were built in the U.S.
and by Slingsby in Great Britain. The ship has
appeared with all three tail styles : the
original had the Schreder V-tail, Slingsby
produced the ヨ14C version with 18 m. wing and
conventional tail, and the ヨ14T version used the
C wing tieh a T-tail. The Slingsby HP-14Cメs are
ATCメd. The type features a 90 degree landing flap
for approach control, originally operated by a
rack and pinion mechanism. The ヨ14C adopted a
rechargeable pneumatic system to ease aerodynamic
operating loads at high speed. Specifications in
parenthesis are for the HP-14T. As with many
homebuilts, a number of builders have made design
changes to their ships. In some cases these have
been substantial. Andre Krutchkoff built his SHP-
1 with his own design of fuselage with T-tail.
Paul Bikle produced a modified ヨ14 (the T-6) with
a 17.37 m./ 57 ft. span wing and control system
modifications. Otto Zauner constructed an 18 m.
model (called the Zauner OZ-4) which has been
modified substantially to have tip extensions
with winglets to give a span of 19.2 m. / 63 ft,
and a gross weight of 386 kg./ 850 lb.
Your Comments:
Sailplanedirectory.com Copyright 2006 Activate Media. Glider data contains
information Copyright www.ssa.org.