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MYASISHCHEV M-17 Stratosfera

From SKYbrary Wiki

Name M-17 Stratosfera
Manufacturer MYASISHCHEV
Body Narrow
Wing Fixed Wing
Position High wing
Tail Booms with twin fins
WTC Light
Type code L1J
Engine Jet
Engine count Single
Position Both sides of fuselage
Landing gear Tricycle retractable
Mass group 3

Manufacturered as:

MYASISHCHEV M-17 Stratosfera

MYASISHCHEV M-17 Stratosfera

MYASISHCHEV M-17 Stratosfera MYASISHCHEV M-17 Stratosfera 3D


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 40.7 m133.53 ft
Length 24 m78.74 ft
Height 4.8 m15.748 ft
Powerplant 1 x 117.2 kN Kolesov RD-36-51
Engine model Kolesov RD-36-51

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
(to FL100)
Descent (FL100
& below)
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 405 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance m ROC ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance m
MTOW 1840018,400 kg
18.4 tonnes
Ceiling FL700 ROD ft/min APC
WTC L Range NM

Accidents & Serious Incidents involving M17

None on SKYbrary