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Page Title:
Valve,Starter Control Aircraft Engine,for TF30 Engine |
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|  MIL-V-81995/2(AS)
25 June 1980
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MILITARY SPECIFICATION SHEET
VALVE, STARTER CONTROL
AIRCRAFT ENGINE, FOR TF30 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-81995.
REQUIREMENTS:
See Figure 1.
Envelope:
weight:
8.0 lb maximum
Aircraft Model:
F-14
Engine Model:
TF30
Operating Inlet Air Conditions:
256 psia
Rated Pressure:
823F (440C)
Rated Temperature:
Maximum Pressure:
280 psia
1020F (550C)
Maximum Temperature:
256 psia
Maximum Engine Interbleed Pressure:
16 psig
Minimum Pressure:
Regulating Pressure: 37.0 + 2.5 psig at inlet pressures from 39
to 241 psig at airflows from 50 lb/rein to 200 lb/rein.
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 or nozzle inlet conditions of 100 0.5 in. Hg abs and 345
10F (174 6C).
Page 1 of 4
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