R-11, Tumansky
Two-spool axial flow turbojet, lightweight design with small frontal area.
R-11B-300
1959
?
turbojet
3900
kg
Yak-25RV
Yak-25RV-I
Yak-25RV-II
Yak-25RRV
Yak-25PA
R-11-?
?
a.b. turbojet
5100
kg
??
MiG-21PF
Ye-2A
Ye-5
R-11AF-300
?
a.b. turbojet
5750
kg
Yak-28
R-11AF-2-300
?
a.b. turbojet
5950
kg
Yak-28R
R-11F
?
a.b. turbojet
5950
kg
MiG-21 (pre-prod)
T-5
Yak-28P
Ye-152A
R-11F-300
R-11-F2S-300
1960
?
a.b. turbojet
6200
kg
MiG-21FL
T-58
Links:
R-11-300, R-11AF-300, R-11AF2-300, R-11F-300, R-11F2-300, R-11F2S-300, R-11V-300
Back to
Main Gate