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| MIL-T-18232B(AS)
3.10.11.3
COOLING AIR CONTROLS. - When air flow around the engine is
required, automatic controls shall be provided for regulating
the cooling air flow with minimum cooling drag.
3.10.12
STARTING SYSTEM
STARTER
3.10.12.1
3.10.12.1.1
RECIPROCATING ENGINES. - Starting shall be accomplished as
specified in the engine model specification.
3.10.12.1.2
TURBO-JET ENGINE. - The starter with necessary accessories
and the priming system shall be subject to the approval of
NAVAIR. The design requirements for starter wiring, fuses} switches, and circuit
breakers, not integral with the starter assembly itself, are included under
"electrical".
3.10.12.1.3
PULSE-JET ENGINE. - The contractor shall make provision for
the use of ground portable equipment for starting the pulse-
jet engine. This equipment consists essentially of a source of compressed air
and the means of applying it to the engine.
3.10.12.1.4
ROCKET ENGINE AND OTHER ENGINE TYPES. - Rocket engines and
other engine types shall be equipped with a starting or
ignition device and the accessories specified in the detail specification.
3.10.12.1.5
STARTING SEQUENCE (PULSE-JET LIQUID AND SOLID ROCKETS
AND OTHER ENGINEER PROPULSION TYPES). - Special consideration
shall be given
to simplicity of the starting sequence.
3.10.12.2
PRIMING SYSTEM (RECIPROCATING). - Priming maybe accomplished
manually or electrically as specified in the detail specifica-
tion
3.10.13
PROPELLER
3.10.13.1
PROPELLER COMPONENTS (RECIPROCATING ENGINES). - The propeller
includes the propeller proper (blades, hub assembly, bolts}
propeller attaching parts, etc.), and spinner.
3.10.13.2
TYPES. - Propellers shall be of the fixed or automatic pitch
type and shall be of wood or metal construction as specified
in the detail specification. Fixed pitch wooden propellers shall be in accordance
with Specification MIL-P-26366. Metal propellers shall be in accordance with
specification MIL-P-26366.
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