 |
|||
|
Page Title:
Starter, Aircraft Engine, Air Turbine, Model A-19-1 |
|
||
| ||||||||||
|
|  MILITARY SPECIFICATION SHEET
STARTER. AIRCRAFT ENGINE, AIR TURBINE, MODEL A-19-1
The complete requirements for procuring the air turbine starter
described herein shall consist of this document and the issue in effect
of Specification MIL-S-19557C (AS).
APPLICABLE
PARAGRAPH OF
SPECIFICATION
Envelope:
Figure 1
3.8.1
Wt. Max (Lb): 25
3.7
Aircraft Model: A-4
6.3.1
Engine Model: J-52
4.5.16
Quick-Attach-Detach Mounting: Yes
3.8.2.1
3.8.2.2
Air Inlet and Exhaust Connections: Figure 1
3.8.3
Rotation Viewed from Anti-Drive End: Clockwise
3.5.5
3.9.1
3.3.2
Ambient Temperature Operating Range (F): -65 to +160
3.3.2
3.3.2.3
Control Valve:
Opening Rate, Max: 22psig per sec for the first .1 sec
4.5.1.1
Closing Time, Max: 0.5 sec
4.5.6
Navy Model: ATSCV-1
3.5.1
Rated Conditions:
Output Drive Speed (RPM): 1100
Output Drive Torque, Min (Lb-ft): 195
Airflow, Max (Lb per Min): O
Air Inlet Total Pressure (In.Hg A): 100
Air Inlet Total Temperature (F): 350
Cutout Speed(RPM): 3450 250
|
|
Privacy Statement - Press Release - Copyright Information. - Contact Us |
Click
here for thousands of PDF manuals