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Page Title:
Valve,Starter Control,Aircraft Engine, for J52 Engine |
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|  MIL-V-81995/3(AS)
25 June 1980
MILITARY SPECIFICATION SHEET
VALVE, STARTER CONTROL,
AIRCRAFT ENGINE, FOR J52 ENGINE
This specification is approved for use by the Naval
Air Systems Command, Department of the Navy, and is
available for use by all Departments and Agencies
of the Department of Defense.
The complete requirements for procuring the starter control valve described
herein shall consist of this document and the latest issue of Specification
MIL-V-8l995.
REQUIREMENTS:
Envelope:
See Figure 1.
Weight:
8.0 lb maximum
Aircraft Model:
EA-6B
Engine Model:
J52
Inlet Air Conditions:
Rated Pressure:
55 psia
Rated Temperature:
350F (177C)
Maximum Pressure:
280 psia
Maximum Temperature:
1000F (538C)
Maximum Engine Interbreed:
259 psia
Minimum Pressure:
16 psig
Regulating Pressure:
37.0 2.5 psig at inlet pressures from 39
psig to 241 psig.
Flow: The flow rate for all test conditions shall be limited by
fixed orifice or nozzle which will produce an airflow of 100 10 lb/rein
at orifice and nozzle inlet conditions of 100 0.5 in Hg abs and 345
10F (174 6C).
Page 1 of 4
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