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PIK-20
E
Flight
manual
'N
7.2.6
Ceiling
With
0.5
m/s
rate
of
climb
(see
Fig
7.3)
W
=
470
kg
h
max
=
5200
m
(17000
ft)
W
=
360
kg
h
max
=
7200
m
(23500
ft)
7.2.7
Operating
range
At
cruising
speed
135
km/h
and
1000
m
(3300
ft)
altitude
the
operating
range
is
230
km
(125
miles)
without
reserve.
The
flight
can
also
be
done
with
dolphin
techie,
ie.
climb
with
max
continous
power
at
100
km/h
to
max
altitude,
then
retract
the
engine,
glide
to
starting
altitude
and
make
a
new
climb
to
max
altitude.
The
ran
ge
can
be
extended
with
this
technic
even
to
450
km
(250
miles).
7.2.8
Thrust
and
drag
with
extended
engine
The
thrust/drag
graph
gives
1.
Sailplane
drag
polars
2.
Drag
polars
with
extended
engine
propeller
windmilling
3.
Drag
polars
with
extended
engine
without
propeller
drag
(to
use
together
with
thrust
curve)
4.
Thrust
curve
with
takeoff
power.
T/D
200
V
(km/h)
FIG
7.6:
Drag
and
thrust
curves
V
EIRI
KY
____
_____________________________
-V
Kisällinkatu
8
SF-15170
Lahti
17
page
I
-48
Revision
1.21.8.-79

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