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Lecture 19: Electric Systems / Power Supply

Electric Power Overview

         Primary Power:  28 VDC

         Secondary Power:

        Isolated from primary power (28VDC)

        CGBA/PGBA: 5VDC, 12VDC, 24VDC, AC-ballasts

         Isolation: = > 1 MegaOhm

        Between different electric circuits to avoid ground loops

        Between video, primary power, secondary power, chassis ground, communication lines

         Bonding:

        Class C:     fault wire (green wire), max. current capable.

        Class H:     all electric components / boxes: < 0.1 Ohm

        Class R:  < 2.5 milli-Ohm

        Class S:  < 1 Ohm

         Grounding:

        Chassis ground (similar ‘green wire’)

        Single Point Ground (SPG) – avoid ground loops / EMI / power loops.

·        Spacecraft: power return is grounded to chassis ground

·        Payload: primary power return must be isolated from chassis, otherwise: ground loops

·        Payload isolated secondary power: must be chassis grounded at single point ground.

         AC / High Voltage Shock Hazard:

        Separation (insulation, potting, inaccessible)

        Current limits (very low)

        Ground Fault Interrupt (or equivalent for space – no ‘ground’).

         Batteries:

        Stored energy, toxic electrolytes

        Leak test with vacuum exposure 6 hrs,

        Current limits / fuses

         Start-up Current

        Inrush current can be very high (charge current for capacitors 100 Amps…..)

·        Soft-start required (short-circuit protection, solid state fuse trips)

·        power supply may trip, or experiment circuit may not start properly – test compatibility.

         Switching power:

        Current: on-resistance of switches: loss = heat = I2 R. very good MOSFET: 0.05W / 10 Amp. = 5 Watt loss

        Voltage: arcing; most consumer electronics: < 30 VDC delta.

Power Conversion

DC Supplies on Spacecraft typical (28VDC Shuttle, 120VDC ISS)

·        Supply may vary (28VDC = 24-32 VDC), but user may need stable voltage à regulation.

·        Voltage loss in lines:  28VDC nominal drops to 19-24V at end of 12 ft cable.

o       MDK Ceiling (10 Amp cb limiting – thermal derating) =19.1 VDC at 9.5 Amp. MAX (182 Watt max.)

o       MDK 10 Amp MUP (10 Amp cb limiting) = 24.0 VDC at 9.5 Amp. MAX (227 Watt max.)

·        DC Regulators: waste heat:  input current = output current, input voltage > output voltage. Loss = heat = (Vin-Vout) * I

·        DC-DC converters: 80-90% efficient; Loss = heat = power used / efficiency = Vout * Iout / n.

o       DC – switched = AC – transformer – rectified to DC – regulated to desired voltage

·        DC-AC Inverters: provide AC voltage (fluorescent lamps, backlighting,….)

o       DC – switched = AC - transformer

·        Isolation between different power circuits may require use of DCDC converters.

·        EMI electromagnetic interference / EMC electromagnetic compatibility: filtering / protection / shielding necessary:

o       radiation / conduction out = emissions

o       radiation / conduction out = susceptibility

o       sample report for PGBA plant chamber (big PDF)

Measurement Instruments:

         Isolation:  > 1 MegaOhm

        Any multimeter with setting > 1 Mohm (10 Mohm)

        Open circuit indication depends on Multimeter

         Grounding / Bonding: < 2.5 mOhm

        Milliohm meter with 4-wire test leads

        6 digit meter with 4-wire test leads

        Multimeter (only check, insufficient resolution)


Design Examples - CGBA Incubator


Plant Growth Chamber

Sample EMI Tests: PGBA Emissions Summary

PGBA Conducted E-Field Emissions

Range

Limits

PVP

Pass/Fail

Plot

CE01-postive lead

30 Hz to 15 kHz

110 @ 30-200 Hz

  74 @ 15kHz

EL-ER-015 2

EL-MD-005

Ö Pass

1

CE01-negative lead

Ö Pass

2

CE03-positive lead

15 kHz to 50MHz

  74 @   15 kHz

  45 @ 500 kHz

  45 @   50 MHz

Ö Pass

3

CE03-negative lead

Ö Pass

4

CE07 (TT01)

Spikes, time domain

 

EL-ER-015 #5, #6, #7

Ö Pass

See fig.

PGBA Radiated E-Field Emissions

 

 

 

 

 

RE02 NB

(SSP52000 and NSST21000) at 1 meter:

 

14 kHz to 20 GHz

 

ISS and NSTS:

 

 

 

RE02NB Narrow Band, vertical polarization,

14k to 1.0GHz

56 @ 14k to 10M

86 @ 259M

46 @ 259M

72 @   10G

76 @ 13.5 - 15.5G

NSTS: 75 @    14k

66 @ 200M

77 @ 10G

EL-ER-015:

#8, #9

@ 1 meter

Ö Pass

5

RE02NB Narrow Band, horizontal polarization,

30M to 200MHz

Ö Pass

6

RE02NB Narrow Band, vertical polarization,

1.0GHz to 10GHz

Ö Pass

7

RE02NB Narrow Band, horizontal polarization,

1.0GHz to 10GHz

Ö Pass

8

RE02NB Narrow Band, vertical polarization,

13.5G – 15.5GHz

Ö Pass

9

RE02NB Narrow Band, horizontal polarization,

13.5G – 15.5GHz

Ö Pass

10

RE02 BB (NSTS21000 only) at 1 meter:

 

NSTS Only:

 

 

 

RE02BB Broad Band, vertical polarization,

14kHz to    1.0GHz

110 @   14k

  65 @ 200M

100 @   10G

  70 @ 1.7-2.3G

 

Ö Pass

11

RE02BB Broad Band, horizontal polarization,

30MHz to 200MHz

Ö Pass

12

RE02BB Broad Band, vertical polarization,

1.0GHz to   10GHz

Ö Pass

13

RE02BB Broad Band, horizontal polarization,

1.0GHz to   10GHz

Ö Pass

14

PGBA AC Magnetic Field Emissions

 

 

 

 

 

RE04, at 1 meter (NSTS only)

30 Hz to 50 kHz

130 @ 30 to 1k

  63 @ 50k

 

Ö Pass

15

RE101 scan for maximum emissions and spectral analysis to locate test locations (Front, top, left, right). Following tests at PEAK for each surface !

30 Hz to 50 kHz

140 @ 30 Hz

  85 @   3.5k

  85 @ 50kHz

 

measured at  7cm.

If exceedances,

Re-measure at 50 cm to pass.

EL-ER-019 #1

PGBA peaks at 30, 50 kHz

Ambient

 

 

16

RE101, Front at LCD screen,  7 cm from faceplate

10,20,30kHz

17

RE101, Front at LCD screen, 50 cm from faceplate

Ö Pass

18

RE101, Left Side,     7 cm from enclosure at peak

Ö Pass

21

RE101, Left Side,   50 cm from enclosure at peak

Ö Pass

22

RE101, Right Side,   7 cm from enclosure at peak

Ö Pass.

23

RE101, Right Side, 50 cm from enclosure at peak

Ö Pass

24

RE101, Top Center,  7 cm from enclosure at peak

Ö Pass

25

PGBA DC Magnetic Field Emissions

 

 

 

 

 

NSTS:  measured at 1 meter

DC

< 170dBpT

EL-MD-006 #2

Ö Pass

N/A

ISS:      measured at 7 cm,

            if fail, measure at 10, 20, 30 cm until below limits.

DC

< 170dBpT

EL-ER-019 #2

Ö Pass

N/A

Note: Plot Number refers to the red hand-written number listed in upper left corner of attached data plots (scanned).


PGBA Susceptibility Summary

Conducted E-Field Susceptibility

Range

Tested Limits

PVP

Pass/Fail

CS01 DC Power Bus Ripple and RF

(positive and negative lead)

30Hz to 2 kHz

2 kHz – 50 kHz

Req.: 0.7 Vrms, falling to 0.28 Vrms; tested at 1 Vrms

EL-ER-016 #2

Ö Pass 10/09/01

CS02 DC Power Bus Ripple and RF

(positive and negative lead)

50kHz to 400 MHz

Req.: 0.28 Vrms

tested at 1 Vrms

El-ER-016 #3

Ö Pass 10/11/01

CS06 DC Power Bus Transients

10ms / 0.15ms, ±28V

6-10 pps, 5 min.

El-ER-016 #4

Ö Pass 10/11/01

NSTS Ripple / Transients – flight (CS01/02 covered)

30 Hz to 400 MHz

» 0.71 Vrms

EL-MD-001

Ö Pass 10/11/01

NSTS Ripple / Transients – ground (CS01/02 covered)

30 Hz to 400 MHz

» 0.71 Vrms

EL-MD-002

Ö Pass 10/11/01

NSTS Hydraulic Pump, 300 ms sawtooth

  500 to 700 Hz

4 Vpp

 

Ö Pass 10/11/01

ISS Ripple / Transients – flight (CS01/02 covered)

10 Hz to   20 MHz

» 0.35 Vrms

EL-ER-007

Ö Pass 10/11/01

Radiated E-Field Susceptibility

 

 

 

 

RS03 Narrowband

14 kHz to 20 GHz

 

 

 

RS03, single polarization

  14kHz to 30 MHz

    5 V/m

EL-ER-016 #6

Ö Pass 10/10/01

RS03, horizontal / vertical polarization

  30M to 200 MHz

    5 V/m

Ö Pass 10/10/01

RS03, horizontal / vertical polarization

200M to     1GHz

  60 V/m

Ö Pass 10/10/01

RS03, horizontal / vertical polarization

     1G to    8 GHz

  60 V/m

Ö Pass 10/10/01

RS03, horizontal / vertical polarization

    8G –  15.5 GHz

  25 V/m

Ö Pass 10/10/01

RS03, horizontal / vertical polarization

        8.5 GHz

  79 V/m

 

Ö Pass 10/10/01

RS03, horizontal / vertical polarization

        2.2 GHz

130 V/m

 

Ö Pass 10/10/01

WCCS Wireless Crew Communication System

338M to 392MHz

    1 V/m

EL-MD-004 #2

Ö Pass

Radiated Magnetic Induction Susceptibility

 

 

 

 

RS02 Radiated Magnetic Induction Susceptibility

 

 

 

 

RS02 – into box / wire wrapped

Pulse 10 ms

±56 V

EL-ER-016

Ö Pass 10/11/01

RS02 – into box / wire wrapped

Pulse   0.15 ms

±56 V

EL-ER-016

Ö Pass 10/11/01

RS02 – into power cables / wire wrapped

Pulse 10 ms

±56 V

EL-ER-016

Ö Pass 10/11/01

RS02 – into power cables / wire wrapped

Pulse   0.15 ms

±56 V

EL-ER-016

Ö Pass 10/11/01

AC magnetic field – Shuttle

30 Hz –   2 kHz

2 kHz – 50 kHz

140 dBpT

falling to 63 dB

EL-MD-004

Ö Pass 10/11/01

AC Magnetic Induced Fields

30 Hz à 50 kHz

140dBpT@7cm

EL-MD-004

Ö Pass 10/11/01

Lightning (covered by RS02)

 

 

 

 

Susceptibility to lightning-induced field, MPLM

 

10A/m

EL-ER-016 #7

Ö Pass 10/11/01

Susceptibility to lightning-induced field, crew compartment

 

  3A/m

EL-MD-004

Ö Pass 10/11/01

Susceptibility to lightning-induced field, protected vehicle

 

  5A/m

EL-MD-004

Ö Pass 10/11/01

Susceptibility to lightning-induced field, unprotect. vehicle

 

10A/m

EL-MD-004

Ö Pass 10/11/01

ESD Susceptibility

 

 

 

 

4000 V: fail safe or no damage, protection

Chassis, connectors

4 kV, powered

EL-ER-017

Ö Pass1 10/11/01

4000 V: fail safe or no damage, protection

Touch Screen

4 kV, powered

EL-ER-017

Ö Pass1 10/11/01

4000 – 15000 V fail safe or no damage, labeling

Chassis, connectors

15 kV, powered

EL-ER-017

Ö Pass1 10/11/01

4000 – 15000 V fail safe or no damage, labeling

Touch Screen

15 kV, powered

EL-ER-017

FAIL2 10/11/01

Note 1:     LCD screen blanked, recovered with reboot / screen refresh from computer, no damage. => pass.

Note 2:    LCD screen blanked, computer rebooted. Static screen remains scrambled, dynamic data display and touch screen operational, screen damaged => fail / requires ESD label or fix to survive ESD air discharge to screen.

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