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1 Microbial Detection Arrays October 23 rd , 2006 Aerospace Senior Projects University of Colorado - Boulder

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Page 1: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

1

Microbial Detection Arrays

October 23rd, 2006

Aerospace Senior Projects

University of Colorado - Boulder

Page 2: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

2

Team Members

• Elizabeth Newton – Project Manager• Shayla Stewart – Systems Engineer• Steven To – Chief Financial Officer• Dave Miller – Fabrication Engineer• Ted Schumacher – Lead Thermal Engineer• Jeff Childers – Lead Structural Engineer• Charles Vaughan – Lead Electrical Engineer• Sameera Wijesinghe - Webmaster

Page 3: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Briefing Overview

• Overall Objectives

• System Design Alternatives

• Design-To Specifications

• Thermal Design Options

• Structural Design Options

• Electrical Design Options

• Project Feasibility and Risk

• Project Plan

• Appendices

Jump to

Look for me for further info

Page 4: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

4

Overall Objectives

Picture from www.physics.byu.edu

Page 5: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Objectives Overview• Objective: To design and build a field-ready unit capable of

providing a testing environment for electrochemical sensors to detect microbial life by soil analysis

• Deliverables:– Field-ready unit– Test data verifying requirements– Operational manual for use

Electrochemical sensors

• Sensors developed by Tufts University and BioServe – Sensors analyze soil for metabolic indicators such as pH and chemical

composition and convert them to electronic signals– Assumes that life only needs water and nutrients found in native soil to

metabolize

Page 6: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Functional Diagram

Geological Sample

Soil Sterilization

Temperature Control

Temperature Control

Test Chamber

Temperature Control

Control Chamber

Inoculation Sample

Reagent Water

Sensors

Data Acquisition and Control

Power

Mixer Mixer

• Accept soil• Sterilize soil using

an autoclave• Add reagent water• Move soil to

reaction chambers• Add non-sterile

inoculation sample to test chamber

• Mix soil and water while starting temperature control

• Testing lasts for two weeks

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Functional Requirements

• Must be capable of performing in extreme Earth conditions– McMurdo Bay, Antarctica

-10°C to 2°C (during summer)

– Atacama Valley, Chile-6°C to 38°C

• Must provide and function with power comparable to next-generation Mars science rovers (30 Watts)

• Must be portable (30 kg)Pictures from Wikipedia.org

Page 8: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Assessment of System Design Alternatives

• Quantitative analysis of cost, mass, and volume based on rough estimates

• Ultimately, complexity became primary consideration

Environmental Controls

Separate

Shared

Separate

Shared

Sterilization Chamber

Overall Architecture:

•Shared Environment

•Separate Sterilization Chambers

Pro-Reaction chambers at same temperature-No need to heat/cool each chamber individuallyCon-No way to correct if one chamber is warmer than the other-More volume to heat/coolPro

-No need for extra environmental chamber

Con

-Each reaction chamber must be heated/insulatedPro-Only one chamber must be fabricated-Only needs one heaterCon

-Soil must be separated into test/control chambers after sterilizationPro

-No need for soil separation: reduced complexityCon

-Two chambers and two heaters

Page 9: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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System Design Alternatives

End Result

• Separate Autoclaves

• Shared Environment

Page 10: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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• Thermal Subsystem– Mass: 16.3 kg– Volume: 0.096 m3

– Cost: $660• Structural Subsystem

(excluding chassis)– Mass: 11.3 kg– Volume: 0.00293 m3

– Cost: $280• Electrical Subsystem

(excluding power supply)– Mass:0.30 kg– Volume:0.00045 m3

– Cost:$1340• Overall System

– Mass:27.9 kg– Volume:0.09938 m3

– Cost:$2280• Total Funds: $8000

Design-To Specifications

Page 11: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Overall System Architecture

Autoclaves

Water Chamber

Pump

DAQ/Power TEC

Inoculation Chamber

Test Chambers

Page 12: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Work Breakdown Structure

MiDAs

Thermal SubsystemStructural Subsystem

Electrical Subsystem

Thermal Control

Insulation

Materials

Soil/Water Transport

Mixing

Power

Data Acquisition

Sensors

Page 13: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Thermal Design Options

Pictures from melcor.com, minco.com, wikipedia.org, energysolutionscenter.org

Page 14: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Insulation Options

• Insulation applications– Autoclave chambers – Environmental chambers – Reagent water chamber– Inoculation sample chamber

• Insulation Requirements– Minimize power needed to heat chambers– Protect electrochemical sensors from heaters

• Criteria (order of importance)1. Volume (thermal conductivity, k)2. Complexity 3. Cost

Page 15: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Insulation Option Pros and Cons

Pros Cons

Silica Aerogel-Very low thermal conductivity

-Expensive

Thermal Coat - Ceramic

-Moisture resistant-Adds almost no volume because it is painted on

-Complicated application

Fiber Board (Sindayno) -350

-Very low density-Thermal conductivity is higher than that of air

Additional Options for Heating and Cooling

Page 16: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Structural Design Options

Pictures from trendir.com, polypenco.co.jp, sonozap.com, sciencelab.com, parker.com

Page 17: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Material Options

• Material applications– Autoclave chambers

• Must be able to withstand high temperatures and pressures

• Must be corrosion-resistant– Environmental, inoculation, and reagent water

chambers • Need to be lightweight

– Reaction chamber• Must be able to be sterilized • Must be inert

• Criteria (order of importance)1. Mass2. Complexity (machineability)3. Cost

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Material Pros and Cons

Pros Cons

Polysulfone

-Low density

-High yield strength

-Easy to machine

-Could not withstand contact with heating elements

-Somewhat expensive

316 Stainless Steel

-High strength

-Very high melting temperature

-Relatively inexpensive

-High density

Ultem 1000

-Low density

-High yield strength

-Easy to machine

-Relatively inexpensive

-Could not withstand contact with heating elements

Additional Options for Soil/Water Transportation and Mixing

Page 19: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Electrical Design Options

Pictures from spectrolab.com, fuelcellstore.com, dpie.com, weedinstrument.com

Page 20: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Power Supply Options

• Power supply requirements– Power supply must provide 30 W of

power– Must power the MiDAs instrument for

duration of experiment (17 days)• Criteria (order of importance)

– Cost– Mass– Volume

Page 21: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Power Supply Pros and Cons

Pros Cons

Fuel Cell -Very high energy density

-Safety and logistic issues

-Switching out tanks

-Expensive

Sealed Lead Acid Battery

-High energy density

-Less complex

-Very large and heavy

-Requires a recharge system

Lithium Ion Battery

-Very high energy density

-High demand

-Requires a recharge system

-Problems holding charge with age

Dual Junction Solar Cells

-Safe, relatively simple

-Can be used to recharge batteries

-Requires sunshine

Additional Options for Data Acquisition and Pressure/Temperature Sensors

Page 22: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Feasibility and Risk

Picture from http://www4.macnn.com/games/gamecenter/risk2/s_01_lrg.jpg

Page 23: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Project Risk Assessment

Subsystem

Mitigation Factors Risk Factors

Lots of Options

Inexpensive

Easy to O

btain

Sim

ple

Easy to M

achine

Lack of E

xpertise

Expensive

Difficult A

nalysis

Hard to O

btain

High P

ower U

se

Thermal Control X X X

Insulation X X X

Material X X X X X

Soil Handling X X X

Mixing X X X X

Power Supply X X X

Data Acquisition X X X

Sensors X X XGreen Subsystems= Low Risk Yellow Subsystems = Medium Risk Red Subsystems= High Risk

Page 24: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Autoclave Feasibility Assumptions

– Fluid inside is only water (high specific heat of water will give maximum boundary)

– Insulation radius = 10 cm of material (thermal conductance of k = 0.012 W/m °C)

– Internal and external losses and safety margin = 2.4W (20% of heating/cooling capacity)

– Specific heat (Cp) for 316 steel = 452 J/kg K– Specific heat (Cp) for water = 4230 J/kg K – Heater uses 12 W per chamber– Standard autoclave techniques implies

• 121°C, hold for 15 min• Cool to 20°C, hold for 24 hours• Repeat 3 times

Page 25: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Autoclave Feasibility Analysis

• Time to heat from -10°C to 121°C = 3.9 hours

• Time to cool to 20°C = 117 min with active cooling

• Power:– 3.9 amp hours to heat– 0.04 amp hours to hold

for 15 minutes– 1.95 amp hours to cool– 3.36 amp hours to hold

for 24 hours

Cm

Wh

22 25

WCRRR convectionconductiontotal 82.79

WR

TTQ

total

gssurroundininside 64.1

QUUU watersteelsys

waterpsteelp TTcmTTcmQ )])()([()])()([( 1212

WC

AhR

outsideconvection 427.0

1

2

Rconduction = kA

Thickness= 79.8 C/W

Page 26: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Autoclave Solution and Verification

• Solution:– Sterilization chamber mock-ups will be

made and tested with various heaters and insulation to verify that it is possible to achieve 121°C

• Verification:– Temperature and pressure sensors will be

used to verify that a sand/water solution can reach 121°C on 30 W of power

Page 27: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Autoclave Power SummaryPower Summary (Sterilization Phase)

0

5

10

15

20

25

30

35

030

060

090

012

0015

0018

00

Operation Time (min)

Po

wer

Co

nsu

mp

tio

n (

W)

Autoclave Heater/Cooler 1

Autoclave Heater/Cooler 2

DAq

Temp/Pressure Sensors

Total Power

Page 28: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Mixing Feasibility Analysis• Requirement:

– Soil and water must be mixed within the reaction chambers

• Reduces boundary layer so electrochemical sensors can read correctly

• Prevents soil sedimentation

• Problem:– Difficult to find mixers small enough to fit in

reaction chambers– Flow pattern difficult to analyze without testing– Unknown if ultrasonic mixers can be used at

appropriate frequency– Magnetic stirrers may affect electrochemical

sensors

Page 29: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Mixing Solution and Verification• Solution:

– Mock-ups of reaction chambers will be prototyped and tested with various mixers

– Different soil granularities will be tested– Various mixing regimes will be tested

• Continuous mixing• Pulsed mixing

• Verification:– Flow patterns and soil sedimentation will be visually

analyzed to show that various types of mixing regimes and mixers provide adequate stirring

Page 30: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Project Plan

Picture from http://www.connectedconcepts.net/clip%20art/Project%20Plan.gif

Page 31: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Organizational Chart

Project ManagerElizabeth Newton

Chief Financial OfficerSteven To

Systems EngineerShayla Stewart

Safety EngineerChuck Vaughan

Fabrication EngineerDave Miller

Thermal Subsystem Electrical Subsystem Structural Subsystem

Thermal LeadTed Schumacher

Dave Miller

Jeff Childers

Shayla Stewart

Electrical LeadChuck Vaughan

Steven To

Structures LeadJeff Childers

Elizabeth Newton

Sameera WijesingheSameera Wijesinghe

Page 32: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Schedule Through CDR

Page 33: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Schedule Through CDR

Page 34: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Schedule Past CDR

• Machining:– Assume one chamber machined per week – Last Machining Day – March 16, 2007

• Testing:– Subsystem testing can begin as soon as each

chamber is constructed– Overall testing: March 16, 2007 – April 17, 2007

• Final Review – April 17, 2007• ITLL Expo – April 28, 2007• Final Report – May 3, 2007

Page 35: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Conclusions

• Project is feasible– Budget is one-quarter of funds – Mass is 34 kg, which is portable– Initial calculations and research indicate that high risk

subsystems (mixing and autoclaving) are challenging but possible

• Further analysis through prototyping will be performed before CDR

– System is capable of performing in specified environments

– System is capable of performing with 30 W of power– Many options are available to meet each requirement

• This allows off-ramps in case some options are dismissed during design

Page 36: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Questions/Comments?

Picture from http://content.answers.com/main/content/wp/en/thumb/5/5b/250px-Nasa_mer_marvin.jpg

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References

1. Cengel, Yunus. Introduction to Thermodynamics and Heat Transfer.

McGraw-Hill. University of Nevada, Reno. 1997

2. Gilmore, David. Spacecraft Thermal Control Handbook. Aerospace press. El Segundo, California. 2002

3. www.aerogel.com

4. www.dimondsystems.com

5. www.matweb.com

6. www.mcmaster.com

7. www.melcor.com

8. www.minco.com

9. www.omega.com

Page 38: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Appendix Table of Contents

• System Architecture Options

• Chamber Geometries

• Verification Methods

• Power Model and Budgets

• Operational Environment

• Subsystem Options, Trade Studies, and Pros and Cons

Page 39: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Appendix A: System Parameter Estimates

Mass (g) Volume (mL) Cost

Reaction Chamber 127 100 $11

Large Autoclave Chamber 4013.5 500 $125

Small Autoclave Chamber 2006.75 250 $63

Soil Transport 88 100 $2.60

Motor 150 200 $20

Moving Sensor Package 254 200 $22

Environmental Sensors 10 50 $200

Page 40: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Assessment of System Design Alternatives

Quantitative Analysis of Options

Mass

(g)

Volume

(mL)

Cost

Shared Environment, Shared Sterilization

900 4444 $150

Separate Environment, Shared Sterilization

1200 4504 $1,350

Separate Environment, Separate Sterilization

1400 4612 $1,750

Shared Sterilization, Separate Environment

1300 4592 $1,350

Mass, volume, and cost figures do not include components that all options need the same number of, such as a reagent water tank and mixers.

Page 41: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Option A• Sterilization and

testing occur in same chamber

• Requires:– 1 large

autoclave– 2 moving sensor

packages– 2 motors– 2 environmental

sensors• High complexity

from moving sensor packages

Mass: 1000 g Volume: 4842 mL Cost: $600

Page 42: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Option B

• Shared sterilization, separate environment

• Requires:– 1 large

autoclave– 2 reaction

chambers– 2 soil transport

tubes

Mass: 900 g Volume: 4444 mL Cost: $150

Page 43: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Option C

• Shared sterilization, separate environment

• Requires:– 1 large autoclave– 2 reaction

chambers– 2 soil transport

tubes– 6 environmental

sensors

Mass: 1200 g Volume: 4504 mL Cost: $1350

Page 44: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Option D

• Separate sterilization, separate environment

• Requires:– 2 small

autoclaves– 2 reaction

chambers– 3 soil transport

tubes– 8 environmental

sensorsMass: 1400 g Volume: 4612 mL Cost: $1750

Page 45: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Option E

• Separate sterilization, shared environment

• Requires:– 2 small

autoclaves– 2 reaction

chambers– 3 soil transport

tubes– 6 environmental

sensors

Mass: 1300 g Volume: 4592 mL Cost: $1350

Page 46: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Autoclave Chamber Geometry

• Assumptions of a possible design: – Chamber is made of 316 stainless steel – 5 mL water added to chamber for use in autoclaving – 15 mL space provided so sample is not tightly packed– Chamber is a cylinder

• Dimensions:– Total internal volume of chamber = 45 mL– Internal diameter = 2.54 cm– External diameter = 3.04 cm– Wall thickness = 0.25 cm – Length = 9.38 cm – Mass = 0.19 km

Page 47: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Reaction Chamber Geometry

• Assume: – Chamber is made of Ultem 1000– Chamber wall thickness of 0.5 cm– Inside chamber geometry is a

cylinder– 20 mL additional space for mixing

(70 mL total volume)• Dimensions:

– Walls: 0.5 cm thick – Outside diameter = 3.95 cm– Height = 11.28 cm – Mass = 0.0866 kg

Drawings by Jake Freeman

Page 48: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Environmental Chamber Geometry

• Assume:– Chamber is a cube

containing both reaction chambers

– Buffer around chambers is 3 cm with 2 cm between them

• Dimensions:– Height: 17.28 cm– Depth: 9.95 cm– Width: 11.95 cm– Volume: 2054.635 cm3

Top View

Side View

Page 49: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Reagent Water Chamber Geometry

• Assume:– Chamber is a cylinder– Water expands upon

freezing• Dimensions:

– Height: 2.1 cm– Radius: 3.0 cm – Volume: 60 cm3Side view

Page 50: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Verification MethodsRequirement

#Title

VerificationMethod

Verification

PDD 4.1Reaction Chamber

VolumeI, D Verification will be through simple volume measurement.

PDD 4.2Reaction Chamber

TemperatureA, T

Verification will be through thermal analysis of the reaction chamber geometry and test by means of simple temperature sensors. 

PDD 4.3Reaction Chamber

PressureA, T

 Verification will be through thermal analysis of the reaction chamber geometry and test by means of simple pressure sensors.

PDD 4.4Reaction Chamber

Sensor CapabilityA, I

 Verification will be through analysis of the chamber geometry and by visual means.

PDD 4.5Reaction Chamber Mixing

CapabilityA, I

 Verification will be through analysis of the flow pattern generated during mixing and basic prototype inspection testing.

PDD 4.6Reaction Chamber Multi-

Use PortA, I

 Verification will be through analysis of the chamber geometry and by visual means.

PDD 4.7Reaction Chamber

MaterialA

 Verification will be through structural and thermal analysis of the reaction chambers.

PDD 4.8Geological Sample

VolumeT

Verification will be through measuring soil before it is added to the autoclave chambers

PDD 4.9Inoculation Sample

VolumeT

Verification will be through measuring inoculation sample before it is added to the inoculation sample chamber

PDD 4.10Inoculation Sample

Reception A, D

Verification will be through analysis of soil transport and demonstration to show sample delivery. 

Page 51: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Verification MethodsRequirement

#Title

VerificationMethod

Verification

PDD 4.11Reaction Sample

HandlingA, T

Verification will be through thermal analysis of the autoclave chambers and testing by means of temperature and pressure sensors. 

PDD 4.12 Inoculation Sample

HandlingA, T

 Verification will be through thermal analysis and testing by means of temperature sensors.

PDD 4.13Reaction Sample

DeliveryA, D

Verification will be through analysis of soil transport and demonstration to show sample delivery.

PDD 4.14 Inoculation Sample

SterilityA, D

  Verification will be through analysis of soil transport and demonstration to show sample delivery.

PDD 4.15Reagent Water Containment

A, T Verification will be through thermal analysis and test by means of temperature sensors.

PDD 4.16 Reagent Water Delivery A, DVerification will be through analysis of soil transport and demonstration to show sample delivery.

PDD 4.17Reagent Water Temperature

A, TVerification will be through thermal analysis and test by means of temperature sensors.

PDD 4.18 Sensor Integration A, IVerification will be through analysis of the reaction chamber geometry and simple volume measurement.

PDD 4.19Sensor Data Collection

RateA, T

Verification will be through analysis and testing of the command software.

PDD 4.20 Sensor Data Acquisition A, TVerification will be through analysis and testing of the command software.

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Verification Methods

Requirement #

TitleVerification

MethodVerification

PDD 4.21Sensor Data Accessibility

D  Verification will be through demonstration of data transfer.

PDD 4.22MiDAs Status

WarningsA, T

 Verification will be through analysis and testing of the command software.

PDD 4.23 MiDAs Command A, T Verification will be through analysis and testing of the command software.

PDD 4.24 Field Power A, T Verification will be through analysis of the power supply and testing through standard electronics lab equipment.

PDD 4.25 Laboratory Power D Verification will be through a demonstration of the instrument with the external laboratory power supply.

PDD 4.26Nominal Power Consumption

A, TVerification will be through analysis of the power consumption of each component and testing. 

PDD 4.27Peak Power Consumption

A, T Verification will be through analysis of the power consumption of each component and testing.

PDD 4.28 Unit Disassembly DVerification will be through a demonstration of the instrument disassembly. 

PDD 4.29 Operational Cycle DVerification will be through a demonstration of a complete operational cycle.

PDD 4.30Operational Environment

AVerification will be through thermal analysis of the surrounding environment. 

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Power Model

Power Summary (Experiment)

0

5

10

15

20

25

012

024

036

048

060

072

084

096

010

8012

0013

2014

4015

6016

8018

0019

20

Operation Time (min)

Po

wer

Co

nsu

mp

tio

n (

W)

Thermal

Structures

Electronics

Total

Page 54: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Mass Budget

Autoclave (316 Steel) x 2 9 kg

Test/control/water chamber (Ultem1000) x 3 2.13 kg

Inoculation chamber (Ultem1000) 0.19 kg

Autoclave Insulation (Aerogel) 13.4 kg

Test/control Insulation (Aerogel) 2.9 kg

DAQ 0.285 kg

Sensors 0.125 kg

Extra (Ultem1000 Chassis) 6 kg

Power supply 4 to 30 kg

Total (excluding power supply) 34 kg

Page 55: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Cost Budget

Heaters x 4 $160

Autoclave (316 Steel) x 2 $240

Test/control/water chamber (Ultem1000) x 3

$40

Inoculation chamber (Ultem1000)

Included above

Autoclave Insulation (Aerogel)

$500 (min purchase)

Test/control Insulation (Aerogel)

Included above

DAQ $995

Sensors $345

Total $2280

Total Funds:

$4000 from Senior Projects

$4000 from BioServe

Total: $8000

Page 56: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Operational Environment

Laboratory

McMurdo Bay,

Antarctica(summer)

Atacama Valley, Chile(Altitude =

2000 m)

Temperature (max)

30°C 2°C 38°C

Temperature (min)

20°C -10°C -6°C

Pressure (avg)

1 atm 1 atm 0.802 atm

Page 57: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Thermal Control Design-To Requirements

Requirement #

Title Requirement Importance

PDD 4.2Reaction Chamber Temperature

Each reaction chamber shall be controllable within a range of 4°C to 37°C with an accuracy of ±1°C.

This environment is acceptable for the possible life to metabolize and reproduce.

PDD 4.11 Reaction Sample Handling

The reaction samples shall be sterilized in accordance with standard Autoclave techniques.

This is the best method of sterilization for killing the known forms of life.

PDD 4.15Reagent Water Containment

The sterile reagent water shall be completely contained in both solid and liquid form.

This prevents the reagent water container from bursting if the water freezes.

PDD 4.17Reagent Water Temperature

The reagent water shall be delivered to the reaction chambers at a temperature not to exceed 60°C.

The electrochemical sensors can't withstand temperatures above 60°C.

PDD 4.30 Operational Environment

MiDAs shall be able to operate in environments ranging from Antarctica to Atacama Valley in Chile.

These are the likely test sites for the MiDAs instrument.

Page 58: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Heating/Cooling Options

• Heating applications– Autoclave chambers: must reach 121°C and hold

for 15 minutes– Environmental chambers: must maintain

temperatures from 4°C to 37°C for 14 days

• Cooling applications– Autoclave chambers – must be cooled from 121°C

to 20°C– Environmental chambers – must maintain

temperatures from 4°C to 37°C for 14 days

• Criteria1. Volume 4. Complexity2. Power consumption 5. Mass3. Risk 6. Cost

Page 59: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Heating Option Pros and Cons

Pros Cons

Strip -Strong sheath -Difficult to find small sizes

Tubular -Good at heating air-Custom length and resistance

needed

Tape or flexible-Cheap-Easy to custom-order-Kapton coating

-Clamping system required-Best used for conduction

heating

Immersion-Direct heating for

substance -Heating element may get in

the way of mixer

Cartridge -High watt density-Requires tight tolerances for

placement

Band -Strong sheath-Small sizes don’t have high

wattages

Page 60: 1 Microbial Detection Arrays October 23 rd, 2006 Aerospace Senior Projects University of Colorado - Boulder

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Cooling Option Pros and Cons

Pros Cons

Passive-Does not require power-Simple

-Geometry of chambers may limit effectiveness-Longest cooling time

Heat Switch-Allows most sides of chamber to be insulated while still allowing cooling

-Complex implementation-Difficult to find data

Thermoelectric Cooler

-Concentrated cooling power-Allows most sides of chamber to be insulated while still allowing cooling

-Requires power

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Heating Options

Heating application

Typical off the shelf example

Power of example

Overall Size of example (inches)

Weight of example

(lbs)

Price of example

Strip Gases or solid surfaces

Omega PT-512/120

2.5W at 12V 5.5 x 1 x 1.5 0.4 $30

Tubular Gases Omega TRI-1212/120

3.3W at 12V 0.246 O.D.x 12 long

0.2 $28

Tape or flexible Solid surfaces or possibly gases

Minco HK5464R4.9L1

2A

29.39W at 12V

3 x 3 0.01 $33.80

Immersion Liquids Omega RI-100/120

2W at 12V Internal heating component =

tube 1.5 long x 0.625 O.D.

3 $115

Cartridge Solids Omega CSS-01235/120

0.7W at 12V 0.124 O.D. x 2 long

0.06 $26

Band Solids in cylindrical form

Omega MBH-1215200A /120

4W at 12V 1.25 I.D. x1.5 width

0.87 $32

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Cooling Options

Typical off the shelf example

Power of example

Overall Size of example

(inches)

Weight of example

(lbs)

Price of example

Passive Cooling

NA 0 0 0 $0

Heat Switch Starsys Research

Diaphragm Thin Plate

Switch

May not be available at this time

Thermoelectric Cooling

Melcor CP1.0-127-05L-1-W5

16 W 30 mm x 30 mm x 3.2 mm

0.024 $15.54

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Insulation Options

Density (kg/m^3) Cost K (W/m-K)

Silica Aerogel 5-200$325 for 50 g + $30

shipping0.016-0.03

TC- Ceramic Unknown Unknown 0.097

Fiber Board (Sindayno) -350 1900 Unknown 0.63

Air 1.168 NA 0.025

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Material Design-To Requirements

Requirement #

Title Requirement Importance

PDD 4.7Reaction Chamber Material

Each reaction chamber shall be manufactured out of a list of materials provided by BioServe. This list includes, but is not yet limited to, Polysulfone, Pharmed, 316 stainless steel, and Ultem 1000.

All of these materials are able to be autoclaved, have high resistance to corrosion, and are FDA approved for food service or medical use.

PDD 4.11Reaction Sample Handling

The reaction samples shall be sterilized in accordance with standard Autoclave techniques.

This is the best method of sterilization for killing the known forms of life.

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Material Options

Density

(g/cm3)

Yield Strength

(MPa)

Maximum Temperature

(°C)

Cost per kg Machineability

Polysulfone 1.24 74.9 149-180 $5.93 Very good

316 Stainless

Steel

8.027 205 899 $2.32 Fair

Ultem 1000 1.27 110 170 $3.84 Very good

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Soil Handling Design-To RequirementsRequirement # Title Requirement Importance

PDD 4.8 Geological Sample VolumeEach reaction chamber shall receive no less than 5 mL and no more than 25 mL of geological sample.

5 mL is the about the minimum amount of soil to obtain good results. 25 mL is still small enough amount to keep the experiment light and portable.

PDD 4.9 Inoculation Sample VolumeThe test chamber shall receive a maximum of 1 mL of inoculation sample.

The nonsterile inoculation sample is what could contain life.

PDD 4.10 Inoculation Sample Reception

The test chamber shall receive the inoculation sample through established aseptic techniques.

The user needs to know that any detected life forms were already present in the soil, not transferred to the soil through the transportation method.

PDD 4.13 Reaction Sample Delivery

One pre-measured reaction sample shall be delivered to the test chamber and one pre-measured reaction sample shall be delivered to the control chamber. Both samples shall maintain sterility throughout delivery.

Having equal amounts of soil in each reaction chamber helps maintain uniformity between the test and control. Once the soil is sterilized, it has to remain sterile so that no life forms are introduced.

PDD 4.14 Inoculation Sample SterilityThe inoculation sample shall be aseptically delivered to the test chamber.

The inoculation sample can't pick up any living organisms from the MiDAs instrument. If life is detected, one needs to know that it was originally in the soil or the experiment is useless.

PDD 4.16 Reagent Water Delivery

The MiDAs shall aseptically deliver no more than 50 mL (within ± 5% accuracy) of sterile reagent water to each reaction chamber.

The delivery must be aseptic, so that no living organisms are transferred to the reagent water.

PDD 4.28 Unit DisassemblyMiDAs shall be able to be taken apart so that it may be sterilized and reassembled for multiple Earth tests.

The instrument needs to be reusable.

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Soil/Water Transportation Options

• Soil and water transportation includes pumps, tubing, and valves

• Soil/water handling applications– Reagent water transferred to sterilization and

inoculation chambers to flush soil– Soil and water mixture transferred from

sterilization and inoculation chambers to reaction chambers

• Criteria1. Complexity (autonomy)

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Soil/Water Transportation Pros and Cons

ProsCons

Push/Pull Solenoids

-Simple -Low cost

-High reliability -Small-Not variable

Electromagnets-Simple -Med cost

-High reliability -Small-High power usage

Motor-Compatibility -Low cost

-Small

-Complexity

-Low reliability

Pressure Sealing

-High reliability

-Two way-Complex setup

Magnetic Sealing

-Less parts

-Low reliability -Complex setup

-One way

-May have interference with sensors

Gat

esS

eali

ng

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Soil Transportation Options

Gate Options Voltage Power Complexity Reliability Size

Push/Pull Solenoids 3VDC 3W low high d = 25.5mm h = 28.9mm

Electromagnets 12VDC ? low high d = 35mm h=~45mm

Motor System

Motor 12VDC 58 RPM low high d =6.3 mm

Belt System N/A N/A high med custom

Sealing Options for Autoclave

Pressure Sealing

Pressure Plug N/A N/A low high custom

Push/Pull Solenoid 3VDC 3W low high d = 25.5mm h = 28.9mm

High Torque Motor TBD TBD low high d = 127mm h = 127mm

Belt System N/A N/A high med custom

Magnetic Sealing

Electromagnets 12VDC ? high high very large

High Compression Spring N/A N/A high low custom

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Mixing Design-To Requirements

Requirement #

Title Requirement Importance

PDD 4.5

Reaction Chamber Mixing Capability

Each reaction chamber shall have mixing capability such that each geological sample is evenly distributed within the fluid while movement is present at each sensor location.

The fluid must be mixed so that the sensor readings are as accurate as possible. The fluid must also move at each sensor so that the boundary layer around the sensors is broken down, which is necessary to get a reading.

PDD 4.28Unit Disassembly

MiDAs shall be able to be taken apart so that it may be sterilized and reassembled for multiple Earth tests.

The instrument needs to be reusable.

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Mixing Options

• Mixing applications– Soil in reaction chambers must be stirred

• Electrochemical sensors need fluid movement to function

• Prevents sedimentation to soil

• Criteria (order of importance)1. Volume2. Power usage3. Risk4. Cost

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Mixing Option Pros and Cons

ProsCons

Ultrasonic-BioServe may provide

-Does not disrupt ISE’s

-Ruptures cell membranes above 18 kHz

-Expensive

-Lack of prior experience

Magnetic

-No known machining required

-Does not require probe through top or bottom of reaction chambers

-ISE interference pending test

-Magnetic Martian soil

Mechanical

-Known flow-pattern

-Does not disrupt ISE’s

-Common use / more experience

-Soil could clog mechanism

-Most COTS mixers are too large

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Mixing Options

Volume Cost Power

Ultrasonics PCB: 5" x 2 3/4" x 1" $1295* variable

  Probe: 0.850" diam, 4 1/2" long    

 Probe tip: 1/8" diam x 2" long Ti

alloy   

Magnetic 4.8” x 4.8” x 1.8”  Unknown

Mechanical 0.8 mm diameter impeller Unknown 

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Power Supply Design-To Requirements

Requirement #

Title Requirement Importance

PDD 4.24 Field PowerMiDAs shall provide its own power (between 10 W and 30 W) in a field setting.

MiDAs shall provide its own power (between 10 W and 30 W) in a field setting.

PDD 4.25Laboratory Power

MiDAs shall be capable of receiving between 10 W and 30 W from an external power supply in a laboratory setting.

The instrument needs to be capable of running in a lab, as well as the field.

PDD 4.26Nominal Power Consumption

Nominal power consumption shall not exceed 30 W.

This is based on estimates of the Mars astrobiology rover

PDD 4.27Peak Power Consumption

Peak power consumption shall not exceed 30 W for more than 30 seconds.

This is based on estimates of the Mars astrobiology rover

PDD 4.29Operational Cycle

One operational testing cycle shall be 14 standard Earth days, not including power-up, sterilization, and power-down.

This is the time given for the potential life to reproduce and metabolize.

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Power Supply Options

Mass (kg) Volume (cm3)

Cost Power Provided

Time for Delivery

Fuel Cell 1.133 637 $1769 30W @ 12V

3-4 Weeks

Sealed Lead Acid Battery

30 10577 $165 40 hrs, 30W @ 12

V

2-3 Weeks

Lithium Ion Battery

8 4800 $40 30 W @ 12V

2-3 Weeks

Dual Junction Solar Cells

0.118 kg (does not include

backing)

Area = 30 cm2

$940 (to charge)

30 W @ 12 V

2 Weeks

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Data Acquisition Design-To Requirements

Requirement # Title Requirement Importance

PDD 4.4 Reaction Chamber Sensor Capability

Each reaction chamber shall be capable of supporting no fewer than 6 and no more than 18 electrochemical sensors.

This is the number of electrochemical sensors that will be provided by the customer.

PDD 4.19 Sensor Data Collection RateThe electrochemical sensors shall have a data collection rate of 1 measurement per minute per sensor.

Since the experiment takes place over 14 days, a reading each minute from each sensor is sufficient to characterize the experiment results.

PDD 4.20 Sensor Data AcquisitionAll data taken through the sensors shall be collected and stored for analysis.

The data will be analyzed after the experiment is completed.

PDD 4.21 Sensor Data AccessibilityThe scientific and engineering status data shall be accessible to users throughout the experiment.

The customer would like to be able to look at the status of the experiment while it is in progress.

PDD 4.22 MiDAs Status WarningsMiDAs shall provide caution, warning, and instrument status to external ground support equipment.

This is necessary to be able to observe the status of the instrument, as well as detect errors.

PDD 4.23 MiDAs CommandMiDAs shall receive commands from external ground support equipment.

The duration of the experiment is such that it is not reasonable to have the user initiate each step of the process.

PDD 4.29 Operational Cycle

One operational testing cycle shall be 14 standard Earth days, not including power-up, sterilization, and power-down.

This is the time given for the potential life to reproduce and metabolize.

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Data Acquisition Options

• Data acquisition applications:– Must be able to give commands to

sensors, heaters, and soil transport– Must be able to store data with a

collection rate of one sample per sensor per minute

• Criteria:– Power usage– Cost

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Data Acquisition Options

DAQ Cards

model power price Weight Width Length Height Resolution Memory Time

LabJack UE95 V or by

USB cable$429 --- 75mm 185mm 30mm 16 bit ---

2 week shipping

LabJack U3by USB cable

$99 --- 75mm 115mm 30mm 12 bit ---2 week shipping

Embedded CPU with DAQ

Athena 10 W $825 150 g 4.175" 4.45" --- 16 bit 128 MB2 week shipping

Poseidon 3.5 W $995 --- 4.528" 6.496" --- 16 bit 256 MB2 week shipping

Elektra 5.5 W $750 108 g 3.55" 3.775" --- 16 bit 128 MB2 week shipping

Hercules 12 W $500 285 g 8" 5.75" --- 16 bit 128 MB2 week shipping

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Data Acquisition Pros and Cons

Pros Cons

Data Acquisition Card

-Self powered (draws power from computer)

-Requires additional hardware

Embedded CPU w/ Data Acquisition

-Embedded system

-Can provided variety of data transfer options

-Can be used to store data until testing complete

-Can provide accessibility to autonomous control

-Requires additional power consumption

-Expensive

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Pressure and Temperature Sensor Options

• Pressure and temperature sensor applications:– One of each sensor in the sterilization chambers

capable of withstanding high temperature– One of each sensor in the each reaction

chamber– One temperature sensor in the reagent water

chamber• Criteria:

– Cost– Power usage– Temperature range

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Temperature Sensor Pros and Cons

Pros Cons

Thermocouples

-Variety of types and configurations

-Low cost, wide availability

-Reliable

-Self-powered

-Can handle autoclave temperatures

-Requires a cold junction compensator for calibration

-Sensor accuracy can reach 1°C at temperatures between 10°C and 40°C

Thermistors-Better accuracy than thermocouples and RTDs

-Loss of linearity

-Requires shielding from high temperatures

-Requires current

Resistance Temperature

Detectors (RTD)

-High accuracy

-Excellent stability and reusability

-Can be immune to electrical noise

-Requires shielding from high temperatures

-Requires current to take measurements

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Temperature Sensor Options

Thermocouples Volume

Model Cost Weight Diameter Length  Temp Range

Operation Range

Accuracy (1-40 °C)

Time

5SRTC-TT (mini connector)

$54 (5 pack)

--- 0.51mm 1m   T --- ±1 °C2 day shipping available

TJ36 (autoclave probe)

$92 --- 1.6mm 1m   JKTE --- ---2 day shipping available

Thermistor

44005 $15 --- 2.8mm 60mm-80 to 250 °C

--- ±1 °C2 day shipping available

RTD Height Length Width

SA1-RTD $50 --- 25mm 2m 19mm-73 to 260 °C

--- ±0.5 °C2 day shipping available

CJC Height Length Width        

MCJ-T (battery included)

$99 57 g 13mm 75mm 25mm T 10-45 °C ---2 day shipping available

CJ-T (battery included)

$170 75 g 12mm 75mm 49mm T 10-50 °C ---2 day shipping available

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Pressure Sensor Pros and Cons

Pros Cons

Gauge-Widely available

-Relatively cheap

-Measures pressure relative to standard atmosphere

Absolute

-Measures pressure relative to vacuum

-Widely available

-Relatively cheap

-Requires additional sensors to measure local conditions

Differential-Measures difference between two locations

-Slightly more expensive than gauge and absolute

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Pressure Sensor Options

Pressure Sensors Volume

Model Cost Weight Height Length WidthTemp Range

PowerAccuracy ***

Time

PX138 * $85 --- 26.2mm 28.1mm 27.9mm0 to 50

°C8VDC

0.1% 0.5%

1 week shipping

PX139 * $85 --- 26.2mm 28.1mm 27.9mm0 to 50

°C5VDC @2 mA

0.1% 0.5%

1 week shipping

PX140 * $120 --- 26.2mm 28.1mm 27.9mm-18 to 63 °C

8VDC0.75 % 0.15%

1 week shipping

      Diameter Length          

PX209 ** $195 --- 12mm 57.9mm  -54 to 121 °C

24VDC @ 15 mA

0.25% 0.25%

1 week shipping