M17

MYASISHCHEV M-17 Stratosfera

Aircraft
Name
M-17 Stratosfera
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
High wing
Tail
Booms with twin fins
WTC
L
Type Code
L1J
Engine
Jet
Engine Count
Single
Position
Both sides of fuselage
Landing gear
Tricycle retractable
Manufacturered as
MYASISHCHEV Stratosfera
MYASISHCHEV M-17 Stratosfera

M17

The design of the Chaika was adapted as a reconnaissance aircraft and emerged as the Myasishchev M-17 Stratosphera with a revised airframe, including straight tapered wings with 2° 30' anhedral (0° at 1g), shorter fuselage pod and unreheated Kolesov RD-36-51 turbojet engine.

Technical Data
Wing span (metric)
40.70 m
Length (metric)
24.00 m
Height (metric)
4.80 m
Powerplant

1 x 117.2 kN Kolesov RD-36-51

Engine Model(s)
Kolesov RD-36-51
Indicative Performance Data
Take-Off
V2
n/a
Distance
n/a
MTOW
18400 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
n/a
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
405 kts
MACH
n/a
Ceiling
700
Range
n/a
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
n/a

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