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Page Title:
Launcher interface requirements. |
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|  MIL-G-85299(AS)
115 v, 400 Hz, phase A power
c.
(1) Launcher - W1, P2-1
(2) Pylon - W2, P2-9
(3) Description: Input power for test set, 105 to 122 vat, 380 to 420
Hz, 120 volt-amperes; fused at two amperes.
d.
Missile identification output, 28 vdc
(1) Launcher - W1, P2-17
(a) Output switched ON/OFF by front panel MISSILE ID switch.
(b) Output voltage shall be the greater of the input Heater
Filament voltage (W1, P2-18) minus a maximum of one volt
dc, or the input Missile Filament voltage (W1, P2-22) minus
a maximum of one volt dc.
(c) External load resistance shall be not less than 1K ohms.
(2) Pylon - W2, P2-13
(a) Output switched ON/OFF by front panel MISSILE ID switch.
(b) Output voltage shall be equal to the 28v bus (W2, P2-15) input
voltage minus not greater than one volt dc.
(c) External load resistance shall be not less than 1K ohms.
All signals - capacitance from interface pin to ground shall be not
e.
greater than 0.6 uf unless otherwise stated.
f.
When between detent positions of the FUNCTION SELECT switch, the STRAY
ENERGY GO lamp shall illuminate and the STRAY ENERGY NO-GO lamp shall
not illuminate.
3.4.5.2 Launcher interface requirements.
a.
FUNCTION SELECT test one.
(1) Missile B+, W1, P2-33, 175 volts dc.
(a) A 14K 5 percent ohms resistive load shall be continuously
applied between ground and the input pin (W1, P2-33).
(b) A 1.4K
5 percent ohms resistive load shall be applied
between ground and the input pin (W1, P2-33) for a single
nonrepetitive 2.0
0.5 second period, after placing the
FUNCTION SELECT switch to position one.
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