One-shot Device
|
Reliability
(i.e., Probability of Successful Operation)
|
95
Confidence Limits
|
Failures per 106 Trials
(See Note 1)
|
---|---|---|---|
Acutator, hot gas
|
0.9983
|
0.9992
0.9960
|
1750
|
Cartridge, Ejector Release Unit
|
0.9992
|
0.9998
0.9972
|
760
|
Cartridge, Cover Removal
|
0.9897
|
0.9965
0.9700
|
10350
|
Expansive Motor: Motor, Gas Piston, Thruster
|
0.9998
|
0.9999
0.9992
|
150
|
Flare, guided missile
|
0.9994
|
0.9999
0.9986
|
566
|
Gas Generator (actuator or remote gyro)
|
0.9988
|
0.9990
0.9985
|
1154
|
Gyro assembly, remote (efflux of remote gas
|
0.9991
|
0.9999
|
928
|
generator impinges on buckets cut into rotor
|
|||
periphery. Reliability of gas generator and
|
|||
igniter not included)
|
|||
0.9976
|
|||
Gyro assembly, integral (cordite charge built
|
0.9936
|
0.9964
|
6359
|
into periphery of rotor; Catherine wheel prin-
|
|||
ciple)
|
|||
0.9889
|
gniter, electric, bridge wire
|
0.9996
|
0.9999
0.9990
|
430
|
Igniter, fuzehead
|
0.9983
|
0.9991
0.9969
|
1700
|
Ignition and Safety Arming Unit (Rocket
|
0.9903
|
0.9939
|
9745
|
Motor)
|
|||
0.9851
|
|||
*Rocket Motor, case-bonded type (less igniter
|
0.9993*
|
0.9997*
|
666*
|
and electrical supply failures)
|
|||
0.9983*
|
|||
Rocket Motor, loose-cartridge type (includes
|
0.9988
|
0.9993
|
1246
|
igniter and electrical supply failures)
|
|||
0.9978
|
|||
Switch, fusible link
|
0.9992
|
0.9999
0.9957
|
735
|
Thermal Battery, cup and cover type
|
0.9996
|
0.9999
0.9985
|
400
|
Thermal Battery, Pellet: Siconium/barium
|
0.9997
|
0.9999
|
320
|
Chloarte pyrotechnic
|
|||
0.9982
|
|||
Thermal Battery, Pellet: Iron/Potassium
Perchlorate pyrotechnic
|
Typical Warhead Initiation Train,
(surface-to-air or air-to-air), consisting of:
|
0.9929
|
0.9979
0.9768
|
7100
|
||
Wire Guidance Mechanism
|
0.9986
|
0.9991
0.9978
|
1400
|
||
|