5962G9322603QZC View Datasheet(PDF) - Aeroflex UTMC

Part Name

Description

Manufacturer

5962G9322603QZC

MIL-STD-1553A/B Bus Transceiver

Aeroflex UTMC 

TRANSMITTER ELECTRICAL CHARACTERISTICS 1

VCC = 5.0V ±10%

-55°C < TC < +125°C

SYMBOL

VO

PARAMETER

Output voltage swing per

MIL-STD-1553B 3, 5

(see figure 9)

MINIMUM

18

MAXIMUM

27

UNIT

VPP,L-L

CONDITION

Transformer-coupled stub, Figure 8,

Point A; input ƒ = 1MHz,

RL = 70 ohms

per MIL-STD-1553B

6.0

(see figure 9)

per MIL-STD-1553A 5

6.0

(see figure 9)

VNS2

Output noise voltage

differential (see figure 9)

VOS4

Output symmetry

-250

-90

VDIS

Output voltage

-900

distortion (overshoot or

ring) (see figure 9)

-300

CIN 2

Input capacitance

TIZ 5

Terminal input

impedance

1

9.0

20

14

5

+250

+90

+900

+300

15

VPP,L-L

VPP,L-L

mV-RMS L-L

mV-RMS L-L

mVPP,L-L

mVPP,L-L

mVpeak,L-L

mVpeak,L-L

pF

Kohm

Direct-coupled stub, Figure 8, Point

A; input ƒ = 1MHz,

RL = 35 ohms

Figure 7, Point A; input

ƒ = 1MHz, RL = 35 ohms

Transformer-coupled stub, Figure 8,

Point A; input ƒ = DC to 10MHz, RL

= 70 ohms

Direct-coupled stub, Figure 8, Point

A; input ƒ = DC to 10MHz,

RL = 35 ohms

Transformer-coupled stub, Figure 8,

Point A; RL = 140 ohms,

measurement taken 2.5µs after end

of transmission

Direct-coupled stub, Figure 8, Point

A; RL = 35 ohms, measurement

taken 2.5µs after end of transmission

Transformer-coupled stub, Figure 8,

Point A; RL = 70 ohms

Direct-coupled stub, Figure 8, Point

A; RL = 35 ohms

RXEN, TXIHB, TXIN, TXIN; input

ƒ = 1MHz @ 0V

Transformer-coupled stub, Figure 7,

Point A; input ƒ = 75KHz to 1MHZ

(power on or power off; non-

transmitting, RL removed from

circuit).

2

Kohm

Direct-coupled stub, Figure 6, Point

A; input ƒ = 75KHz to 1MHZ (power

on or power off; non-transmitting,

RL removed from circuit).

Notes:

1. All tests guaranteed per test figure 6.

2. Guaranteed by device characterization. Capacitance is measured only for initial qualification and after any process or design changes which may affect

input or output capacitance.

3. For MIL-STD-1760, 22 Vp-p, L-L min.

4. Test in accordance with the method described in MIL-STD-1553B output symmetry, section 4.5.2.1.1.4.

5. Guaranteed to the limits specified if not tested.

11

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