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THEMIS Instrument PDR 1 UCB, October 15-16, 2003 IDPU Mechanical / Thermal Preliminary Design Review Heath Bersch University of California - Berkeley

THEMIS Instrument PDR 1 UCB, October 15-16, 2003 IDPU Mechanical / Thermal Preliminary Design Review Heath Bersch University of California - Berkeley

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Page 1: THEMIS Instrument PDR 1 UCB, October 15-16, 2003 IDPU Mechanical / Thermal Preliminary Design Review Heath Bersch University of California - Berkeley

THEMIS Instrument PDR 1 UCB, October 15-16, 2003

IDPU Mechanical / Thermal

Preliminary Design ReviewHeath Bersch

University of California - Berkeley

Page 2: THEMIS Instrument PDR 1 UCB, October 15-16, 2003 IDPU Mechanical / Thermal Preliminary Design Review Heath Bersch University of California - Berkeley

THEMIS Instrument PDR 2 UCB, October 15-16, 2003

IDPU Concept

IDPU Chassis Concept

MASS = 1800 GRAMS EMPTY

4MM WALLS PROVIDE SHIELDINGADDITIONAL SHIELDING PER BOARDAND SPACE CRAFT BUS

Volume = 652 cubic centimeters

Page 3: THEMIS Instrument PDR 1 UCB, October 15-16, 2003 IDPU Mechanical / Thermal Preliminary Design Review Heath Bersch University of California - Berkeley

THEMIS Instrument PDR 3 UCB, October 15-16, 2003

ICD Drawing

Page 4: THEMIS Instrument PDR 1 UCB, October 15-16, 2003 IDPU Mechanical / Thermal Preliminary Design Review Heath Bersch University of California - Berkeley

THEMIS Instrument PDR 4 UCB, October 15-16, 2003

LVPS

FGE/PCB

DCB/ETC

DFB

BEB

SST

Card Assignments

Page 5: THEMIS Instrument PDR 1 UCB, October 15-16, 2003 IDPU Mechanical / Thermal Preliminary Design Review Heath Bersch University of California - Berkeley

THEMIS Instrument PDR 5 UCB, October 15-16, 2003

ALUM SHIELD

PEM SPACER

HEAT SINKS

WEDGE LOC

D-SUB CONNECTOR

Standard Card

Page 6: THEMIS Instrument PDR 1 UCB, October 15-16, 2003 IDPU Mechanical / Thermal Preliminary Design Review Heath Bersch University of California - Berkeley

THEMIS Instrument PDR 6 UCB, October 15-16, 2003

Wedge Loc Interface

Page 7: THEMIS Instrument PDR 1 UCB, October 15-16, 2003 IDPU Mechanical / Thermal Preliminary Design Review Heath Bersch University of California - Berkeley

THEMIS Instrument PDR 7 UCB, October 15-16, 2003

ESA Attachment Concept

Page 8: THEMIS Instrument PDR 1 UCB, October 15-16, 2003 IDPU Mechanical / Thermal Preliminary Design Review Heath Bersch University of California - Berkeley

THEMIS Instrument PDR 8 UCB, October 15-16, 2003

Thermal - IDPU

Heat Transfer

Power Dissipation

•10.74 W

Conduction

•We are trying to keep the bottom deck warm

•Therefore the IDPU is thermally coupled to the bottom deck using a ChoTherm gasket

•ESA conducts heat away and radiates it to space

Radiation

•All surfaces covered with low ε VDA tape or blankets

•IDPU may need radiator, current Swales model includes one

Page 9: THEMIS Instrument PDR 1 UCB, October 15-16, 2003 IDPU Mechanical / Thermal Preliminary Design Review Heath Bersch University of California - Berkeley

THEMIS Instrument PDR 9 UCB, October 15-16, 2003

Thermal - IDPU

Temperature Limits

•Predictions from Swales

•Cold prediction from 3 hour eclipse orbit

•Hot prediction from hottest orbit and attitude

•Average operating temperature around 30 °C

•Better predictions await more complete instrument thermal models

Survival (°C)Predictions

(°C)

Margin

(°C)Eclipse-Op

Science-Op Cold Hot Cold Hot

-50 -30 40 +65 -16 36 14 4

Page 10: THEMIS Instrument PDR 1 UCB, October 15-16, 2003 IDPU Mechanical / Thermal Preliminary Design Review Heath Bersch University of California - Berkeley

THEMIS Instrument PDR 10 UCB, October 15-16, 2003

Thermal - IDPU

Temperature Monitoring and Control

•Modified Interface Monitoring

•Probe Bus will monitor the interface temperature near the IDPU

•Instrument Monitoring

•IDPU will process additional thermistors if needed

•Heaters

•No operational heaters are required

•Survival heaters will keep IDPU above Eclipse-Op Limits

•Two heater services provided by the probe bus

•Primary service thermostat closes at -23

•Secondary service thermostat closes at –28

•IDPU may share heater with the ESA, depends on final coupling