5962-8864406YC 데이터 시트보기 (PDF) - Aeroflex UTMC

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5962-8864406YC

MIL-STD-1553A/B Bus Transceiver

Aeroflex UTMC 

TRANSMITTER ELECTRICAL CHARACTERISTICS1

VCC = +5V (± 10%)

VCCA = +5V to + 12V (± 5%) or +5V to +15V (± 5%)

VEE = -12V or -15V (± 5%)

-55°C < TC < +125°C

SYMBOL

PARAMETER

MINIMUM MAXIMUM UNIT

CONITION

VO Output Voltage Swing per

18

MIL-STD-1553B 2

(See figure 9)

per MIL-STD-1553B

6

(See figure 9)

per MIL-STD-1553A 2

6

(See figure 9)

VNS 2

Output Noise

Voltage Differential

(See figure 9)

VOS 2

Output Symmetry

(See figure 9)

-250

-90

VDIS 2 Output voltage distortion

-900

(overshoot or ring)

(See figure 9)

-300

27

9

20

14

5

+250

+90

+900

+300

VPP, L-L

VPP, L-L

VPP, L-L

Transformer-coupled stub, Figure

8, Point A: input ƒ = 1MHz,

RL = 70 ohms.

Direct-coupled stub, Figure 8,

Point A: input ƒ = 1MHz,

RL = 35 ohms.

Figure 7, Point A:

input ƒ = 1MHz, RL = 35 ohms.

mV-RMS, Transformer-coupled stub, Figure

L-L 8, Point A: input ƒ = DC to 10MHz,

RL = 70 ohms.

mV-RMS, Direct-coupled stub, Figure 8,

L-L Point A: input ƒ = DC to 10MHz,

RL = 35 ohms.

mVPP, L-L Transformer-coupled stub, Figure

8, Point A: RL = 70 ohms, measure-

ment taken 2.5µs after end of trans-

mVPP, L-L mission

Direct-coupled stub, Figure 8,

Point A: RL = 35 ohms, measure-

ment taken 2.5µs after end of trans-

mission

mV peak, Transformer-coupled stub, Figure

L-L 8, Point A: RL = 70 ohms.

mV peak, Direct-coupled stub, Figure 8,

L-L Point A: RL = 35 ohms.

CIN 2 Input Capacitance

10

TIZ 2 Terminal Input Impedance

1

2

Notes:

1. All tests guaranteed per test figure 6.

2. Guaranteed by device characterization.

13

pF

Kohm

Kohm

TXIHB, TXIN, TXIN; input

ƒ = 1MHz @ 0 V

Transformer-coupled stub, Figure

7, Point A: input ƒ = 75KHz to

1MHz (power on or power off: non-

transmitting, RL removed from

circuit).

Direct-coupled stub, Figure 6,

Point A: input ƒ = 75KHz to 1MHz

(power on or power off: non-trans-

mitting, RL removed from circuit).

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