ATAR 101 E5
air turbine starter
Coleoptère
Coleoptère
Nord Griffon II
Nord Griffon II
1952 SNCASO S.O. 4050-03 Vautour
Dassault Etendard
ATAR 101 G3
1956 Dassault Mirage III-001
Dassault Super Mystère B2
1956 Dassault Super Mystère B2
B1 B2 C D E 08C 1957(+reheat) F G
-9 stage compressor (airflow +15%)-last 3 stages in steel-2-stage turbine-systems below engine-eyelid exhaust nozzles
produced: 176
ATAR 101 E5 8C
year 1956 1957
thrust (lbf) 8160 9700
rpm 8400 8400
TET (C°) 865 885(F°) 1590 1625
pressure ratio: 4.8 5.8
compressor stages: 8 9max. diameter (mm/in):920 / 36.2
1956 Dassault Étendard IV M
ATAR 101 08C
B1 B2 C D E 08C(+reheat) F G 09B 1957
-all compressor stages in steel
lowest specific mass in the world:0.227 lb/lbf - thrust/weight ratio: 4.4
produced: 419
ATAR 101 8C 9B
year 1957 1957
thrust (lbf) 9700 9400(reheat) (13 200)
rpm 8400 8400
TET (C°) 885 885(F°) 1625 1625
pressure ratio: 5.8 5.7
compressor stages: 9 9max. diameter (mm/in):920 / 36.2 1020 / 40.2
ATAR 101 09B
Dassault Mirage IIIC
SEPR 844
SEPR 844
Dassault Mirage IIIO
B1 B2 C D E 8C(+reheat) F G 9B 9C 1960
-multiflap exhaust nozzle-starter: Microturbo Noelle 60
produced: 1671
Microturbo NOELLE 60290
diameter: 312 mmlength: 613 mm
Electric starter:27000 rpm
Turbine engine:47000 rpmFree turbine
Mirage IIICJ
IAI Kfir
Mirage 5
9K50
9K
9C
B1 B2 C D E 8C(+reheat) F G 9B 9C 9K 1961
-first 2 stages transsonic-electronic TET/rpm management
produced: 248
ATAR 101 9B 9K
year 1957 1961
thrust (lbf) 9400 10900(reheat) (13 200) (15 100)
rpm 8400 8400
TET (C°) 885 920(F°) 1625 1690
pressure ratio: 5.7 6.15
compressor stages: 9 9max. diameter (mm/in):1020 / 40.2
101 9K
Dassault Mirage IV