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P14651: Drop Tower for Microgravity Simulation . Adam Hertzlin Dustin Bordonaro Jake Gray Santiago Murcia Yoem Clara. Project Summary. Problem Goals Design & Build Drop Tower Vacuum Piping Structure Cost Effective Effective Cycle Time Aesthetically Pleasing Precision in Measurements - PowerPoint PPT Presentation
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Adam HertzlinDustin Bordonaro
Jake GraySantiago Murcia
Yoem Clara
P14651: Drop Tower for Microgravity Simulation
Project Summary Problem Goals
Design & Build Drop Tower Vacuum Piping Structure Cost Effective Effective Cycle Time Aesthetically Pleasing Precision in Measurements Educational User Interface Access for Object Transfer Adaptability for Future Development
Constraints Location and design approval from the dean(s) Material availability/size (ex. tube, pump) The device is aesthetically pleasing The tower 6” – 12” Diameter The device can be operated year round. The system is safe to operate. The project budget is $3,000. Team must justify the need for additional
funds. The project must be completed in 2 semesters.
Project DeliverablesInstalled drop towerDetailed design drawings and assembly manualBill of materialsUser’s Guide for operationDesigned Lab Experiments
Determine gravity in the vacuum within 1% errorCompare drag at different pressures and drag vs. accelerationAdditional vacuum related experiments
Fun and Educational Experience for Middle School Students
Technical Paper Poster
Week #6 Review Open ItemsWhat are the engineering requirement
values?How is external pressure accounted for?Does Temperature Affect Calculations?
AgendaCustomer Meeting Updates
Customer RequirementsEngineering RequirementsProposed Concept DesignIsolation Valve Cost Analysis
List of experimentsConcept and Architecture DevelopmentSystem Block
Sub-systemsSummary
Risk AssessmentTest PlanBill of Materials
Customer Meeting Notes Account for Pipe Fitting Leaks in calculations
How does Ultimate Pressure change with Leak Rate?Limit design to one tower
Simple PrototypeFit two objects in one tower
Allow for lift mechanismDesign Concepts to Future Tower Development
Go with 6-8 in. Diameter, approx. 10-15 ft. Tall TowerMeasure new location heights
Dr. K LabTalk with Mark Smith about using MSD spaceDoes Ultimate Pressure Effect object drop times
Feather vs. Ball BearingUse only one laser when dropping items to measure gravityKeep the educational aspect in mind
Customer RequirementsCustomer Rqmt. # Importance Description
CR1 9 Appropriate Tower HeightCR2 9 Allow for Adjustable PressureCR3 9 Display Tower PressureCR4 9 Drop 2 objects simultaneouslyCR5 9 Drop objects with no horizontal motionCR6 9 Demonstrate standard local gravity within 1%CR7 9 Display important outputs accuratelyCR8 9 Allow full drop visibility and limit distortionCR9 9 Demonstrate drag vs. pressureCR10 9 Allow objects to be changed outCR11 9 Safe/Intuitive operationCR12 9 Educational and InspiringCR13 3 Display Tower TemperatureCR14 3 Design considers noise and power requirements and limitsCR15 3 Components are properly maintained and storedCR16 3 Aesthetically pleasingCR17 3 Generate object lift mechanism concepts for future MSDCR18 3 Allow for further static experiments
Engineering RequirementsRqmt.
# I Engr. Requirement (metric) Unit of Measure Marginal Value Ideal Value
SR1 9 Measure Relative Object Position ft 0-15 >Tower HeightSR2 9 Measure Relative Object Drop Time sec 0-2 SR3 9 Measure Pressure psi 0-14.7 0 - 14.7SR4 9 Cycle Run Time min 1-10 mins 1 minSR5 9 Pressure Leak Rate Minimized psi / sec 0-? 0SR6 9 Aesthetic Structure with Supports Yes / No Yes YesSR7 9 No Horizontal Motion in 0 - ? 0SR8 9 Tube Collapse Pressure FOS 0-5 5SR9 9 Timing difference of object release millisecond 0 - ? 0SR10 3 Tower Height ft 10-15 15SR11 3 Tower Cross - Section (Diameter) in 6-8 8SR12 3 Pump Flow Rate ft3/min 2-10 10SR13 3 Measure Temperature % Error 0-1 0
SR14 3 Impact Energy Dissipation Method Joule 0-(mmaxvfinal2/2) (mmaxvfinal
2/2)
SR15 3 Air Intake - Tower Pressure Change Rate ft3/min 0 - ? ?SR16 3 Minimal Error in Calculations % error 0 - 1% 0%SR17 3 Aesthetic Data Display Yes / No Yes Yes
SR18 3 Platform for Stationary Experiments in (0.50*ID)-(0.99*ID) (0.99*ID)
Isolation Valve – Cost vs. Time AnalysisTime to Evacuate (min)
No Isolation Valves
Time to Evacuate (min) Isolation
Valves
Price, Single Tower, 2 Isolation
Valves
15ft Tower 40ft Tower 15ft / 40ft Tower 15ft / 40ft Tower
6" Dia. 3.25 8.95 0.86 $4,940.00
8" Dia. 5.72 15.46 1.52 $6,880.00
12" Dia. 12.79 34.25 3.41 $9,984.00
Assumptions: No losses due to connection points, 10 cubic foot per meter pump, 15 micron ultimate pressure, 2ft above & below valves, single tower
Isolation Valves Pros and Cons+
Quicker cycle time The air needed to be
taken out of the pump is independent of tower height Can use less costly pump (Lower pump speed)
- Costly Disrupts view of items
falling Can not alter for a
continuous system in the future
More pipe / pump sections need more parts
More chance of pressure leak
Our Conclusion: Although isolation valves would save a substantial amount of time, the time benefit does not outweigh the cost for the tower height we are considering. At this scale it would be more beneficial to increase the pump size instead.
List of ExperimentsDropping two objects simultaneously Measure Gravity Measure DragBalloon ExpansionMarshmallow ExpansionSound InsulatorPlastic Bottle Compression
Note: The following slides will attempt to justify the required tower pressure and size to complete these experiments
CONCEPT & ARCHITECTURE DEVELOPMENT
Prop
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Prop
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Sele
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Cont
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#1
System Block Diagram
Sub-SystemsI. Release Mechanism
I. Release system CalculationsII. Air Control
I. Ultimate Pressure II. Evacuation time III. Leak Rate Analysis
III. Catching MechanismI. Energy dissipation Calculations
IV. Piping systemI. Critical external Pressure
V. SensorsVI. Structure
I. Tower height calculationsII. Support Buckling
Engineering Analysis Release Mechanism
Base Specifications
1.5” 1.5”
0.375”
4.0”
0.375”
6.0”
Polycarbonate • Diameter = 6.0 in• Thickness = 0.375 in • ρ = 1.22 g/cm3 (0.0441 lb/in3)
Hatch Doors • Length = 1.5 in • Width =4.0 in• Thickness = 0.375 in
Electromagnet SpecificationsElectrical Specifications
• 12 VDC• Operating
temperature of -40F to 140F
• Holding Force 4.5lbsPhysical Specifications
• Weight – 0.06lbs• Diameter – 0.75in• Height – 0.62in
Other Specifications• Quick Release
Mechanism
Hinges SpecificationsPhysical Specifications• Height – 3.5in• Width – 1.5in• Depth – 0.21in• Radius – 5/16in (0.3125in)Pin Specifications• Length – 3.5in• Radius – 9/16in (0.5625in)
FBD
Given ValuesSymbol Value Units
Wo 32.17 Lbf
Wd 3.19 Lbf
Wm 2.90 Lbf
Fmx 6 Lbf
Equations
Force of Magnet in y-direction
Force of Pin in the x and y Direction
Shear Stress
Factor of Safety
Engineering Analysis - Air Control Ultimate Pressure & Gravity Error Effect
Gravity Calculation with 1% ErrorConstant Acceleration Equations
Assumes no air resistance / perfect vacuum
, where x is position and t is time
Assume 0.XX% Error due to pressure
Free Body Diagram of ObjectForce Balance
At Terminal VelocityAcceleration = 0
At Vacuum Pressure, drag force = 0, where a is downward (negative)
Drag Force (Air Resistance)
FD = Drag Force ρ = Air Density V = Velocity of Object CD = Drag Coefficient (Fudge Factor) A = Projected Area of Object
P = Air Pressure (Pa) R = Specific Gas Constant = 287.05 J/kg*K T = Air Temperature = 21°C = 274K
Objects to calculate gravity Based on a certain vacuum pressure and other
parameters, center objects will be suitable of calculations while others are not
Objects vary by their mass, projected area and drag coefficient
Assumptions: Allowable Error in Gravity due to Pressure = 0.01%
This can increase if the error from the position and time measurements are minimized
Pressure = 0.015 Torr = 2 Pa This can be decreased if a more efficient pump is available (cost / benefit)
Max Tube Height = 5 meters Max Velocity Ideal Gas Room Temperature Standard Gravity
ResultsFor the assumptions: Gravity Error = 0.01%
Base Pressure = 2 Pam/(CD*A) >= 1.19 kg/m^2
Where: m = mass (kg) CD = Drag Coefficient A = Projected Area
Note: Error % and Pressure can be adjusted to change this threshold
1" Steel Ball
1.625" Steel Ball
Ping Pong Ball Feather Coffee Filter
Drag Coefficient, CD 0.47 0.47 0.47 1.00 0.75
Projected Area, A (m^2) 0.0005 0.0013 0.0013 0.0026 0.0127
Mass, m (kg) 0.067 0.289 0.003 0.001 0.001
m/(CD*A) 280.46 459.63 4.62 0.39 0.14
0 20 40 60 80 100 1200.00
5.00
10.00
15.00
20.00
25.00
30.00
Object Parameter Limit Based on Ultimate Pressure & Error in Gravity
0.01% Error0.05% Error0.10% Error
Ultimate Pressure (Pa)
m/(CD
*A)
Ping Pong Ball Threshold
Engineering Analysis - Air Control Evacuation Time
Conductance The flow of air in a tube, at constant temperature, is
dependent on the pressure drop as well as the cross sectional geometry.
Viscous Flow: Pressure (micron) * Diameter (in) > 200
Transitional Flow: 6.0 < Pressure (micron) * Diameter (in) < 200 ,
Molecular Flow: Pressure (micron) * Diameter (in) < 6.0C = Conductance (cfm)
F1 = Viscous/Transitional Flow Scale Factor = 0.52 F2 = Transitional Flow Scale Factor = 12.2 F3 = Molecular Flow Scale Factor = 13.6 D = Pipe Diameter (in) L = Pipe Length (ft)
Viscous Molecular
Equivalent Pipe LengthPipe fittings can cause losses within a
piping systemThese include: elbows, tees, couplings,
valves, diameters changes, etc.Tabulated values for Le/D can be used to
adjust L in the conductance equationsD = Diameter of PipeLe = Equivalent LengthTotal Length = L + Le1 + Le2 + Le3 + ….
Effective Pump Speed SEff for each flow regime
Viscous, Transitional, & Molecularn = number of pipe diametersC = Conductance (cfm) = Given Pump Speed (cfm)= Effective Pump Speed for Tube Dimensions
Evacuation Time = 760 Torr (Atmospheric) = Viscous–Transitional Pressure = Transitional-Molecular Pressure = Ultimate Pressure
• Example: Single 6” x 15’ Tube
Pump used on leftSee Spreadsheet for:
• Fittings• Individual conductance• Individual flow regime time
VP6D CPS Vacuum Pump
2 Stage Rotary Pump15 micron Ultimate
VacuumPump Speed – 6.25 cfm
Price: $268.92
ResultsFor the tube and pump size listed, the evacuation time is 5.25 minutesThis will increase if:
Tube diameter increasesTube length increasesPump speed decreasesUltimate pressure decreases
Engineering Analysis - Air Control Leak Rate
Chamber Leak RateThroughput, Q
Units: (Pressure * Volume) / TimePump Throughput, QP
Where: Seff = Effective Pump Speed P = Pressure
Leak Throughput, QL
Where: dP/dt = Differential Pressure V = Chamber Volume
Constants:• Chamber Volume• Temperature• Atmospheric
Pressure• Leak Area
Time Variables:• Mass Flow Rate• Chamber Pressure
Leak
Pump
𝑄𝑃=𝑆𝐸𝑓𝑓 ∗𝑃
V
𝑃 𝐵𝑎𝑠𝑒=
Δ 𝑃Δ𝑡 ∗𝑉
𝑆𝑒𝑓𝑓
0.0 10.0 20.0 30.0 40.0 50.0 60.00.00
5.00
10.00
15.00
20.00
25.00
30.00
How Leakage Affects Ultimate Pressure
Leak Rate (Pa / min)
Base Pressure (Pa)
𝑃𝑈𝑙𝑡𝑖𝑚𝑎𝑡𝑒=2𝑃𝑎=𝑃𝑚𝑖𝑛
Flow Regime Change
Engineering Analysis - Catching Mechanism Energy Dissipation
Energy Dissipation
In process …
Engineering Analysis – Piping System Critical External Pressure
Pipe Critical Pressure Calculations
Desired Factor of Safety = 3-4
P 14.7 psiv 0.37 E 429000 psi
Size (in) OD (in) Thickness (in) Max Pressure (psi) Factor of Safety6 6.625 0.28 85.43 5.818 8.625 0.322 57.98 3.94
10 10.75 0.365 43.16 2.9412 12.75 0.406 35.37 2.41
SCH 40 Pipe Maximum Pressure
Critical Pressure Calculations for Clear PVCFormula
PCrit=(2*E/(1-v^2))*(1/((OD/t)-1)^3)
Pipe Dimensions Courtesy of Engineeringtoolbox.com
Size (in) Max Pressure (psi) Factor of Safety6 90 6.128 58 3.9510 49 3.3312 42 2.86
Max Pressure Rating of Schedule 40 PVC*, from HARVEL
*Specifications for white PVC
Engineering Analysis – Laser SensorSensor
Laser Distance Sensor• Micro-Epsilon ILR-1030• 15m Range• 4-20mA Output• 10ms Response time
Engineering Analysis – StructureTower Height
Free Fall – No Air Resistance (Vacuum Conditions)Applies to All Objects:
Vi=0g=32.2ft/s2
Free Fall –Air Resistance (Atmospheric Conditions)
Fall Time Differs Per Object; Depends on Drag Coefficient, Projected Area and Mass of Object Dropped.
Equations Dependent on Terminal Velocity (Vterm or V∞); The Highest Velocity the Object Reaches, at the Point Downward Acceleration Becomes Zero
Free Fall –Air Resistance (Atmospheric Conditions)
ρ is the Density of Airis the Drag CoefficientA is the Projected Area of the Falling Object
Free Fall –Air Resistance (Atmospheric Conditions)
Tower Height ResultsAssumptions
0.5 – 1.0 drop time difference is adequateSteel Ball Bearing vs. Feather
Result10 – 15ft Tower Height
Engineering Analysis – StructureSupport Buckling
Schematic
• Worst case scenario:– 15’ Long PVC Schedule 40– 8” Diameter– 10’ long square A513 tube
• So 10’ of buckling length
• Assumptions:– Weight of vacuum tube is
split evenly between four connection points
Tube
Frame
Pipe Riser Clamp
Pipe Riser Clamp
Depiction of Reaction Forces on Tube
10ft
W/4
• Becomes an eccentric column loading problem because the weight of the tube is applied on one face of the support columns
• Requires numerical methods root finding techniques
W/4
W/4
W/4
W/2
W/2
Eccentric Distance
Bisection Method using Matlab:function [] = Buckling_Bisection()%Buckling_Bisection finds the value of max applicable load, F, that %the beam may support before collapse. %Calculate tube weight:dens=2.581; %slug/ft^3 http://www.clearpvcpipe.com/pdf/ClearPVCspecs.pdf OD=8.625/12; %OD of pipe in ft (SEE BOM)ID=7.943/12; %ID of pipe in ft (SEE BOM)L=15; %Length of pipe in ftV=(pi()/4)*(OD^2-ID^2)*L; %Volume of pipe in ft^3W=dens*V*32.2; %weight of the pipe in lbfWap=W/4; %weight at each connection point, assuming it's distributed %evenly across two bars with 2 connection points on eact bar %Calculate Pcra=1.5/12; %assuming a square x-section, the width in ftt=.12/12; %thickness of wall in ftb=a-2*t; %inner distace between wallsA=(a*a)-(b*b);l=10; %length in buckling in ftSyc=63100*(12^2); %Yield strength of A513 in lb/ft^3 (MATWEB)E=29700000*(12^2); %Elastic modulus of A513 in lb/ft^3 (MATWEB)e=OD/2+a/2+1/12; %eccentric distance, 1/2 of steel thickness + 1/2 OD of %vacuum tube + distance between edge of steel and vacuum tube c=a/2; %1/2 the distance across the cross-section of the hollow square barI=(1/12)*a*a^3-(1/12)*b*b^3; %Inertia of the bark=sqrt(I/A); %radius of gyrationf=@(F) F/A-Syc/(1+(e*c/k^2)*sec((l/(2*k))*sqrt(F/(A*E))));Fl=1;Fu=10000;Fn=(Fu+Fl)/2;ed=.05;ea=abs((Fu-Fl)/(2*Fn))*100;iter=0;imax=100;while ea>ed && iter<imaxif f(Fl)*f(Fn)<0;Fu=Fn;iter=iter+1;else (f(Fl)*f(Fn))>0;Fl=Fn;iter=iter+1;endFn=(Fu+Fl)/2;ea=abs((Fu-Fl)/(2*Fn))*100;endFr=Fn;FOS=Fr/Wap;%ezplot(f,[1200,2000]); grid minor;fprintf('\n F (lbf) is: %.0f \n FOS is: %.0f \n The percent error is: %.3f \n',Fr,FOS,ea);end
Solution:
>> Buckling_Bisection
F (lbf) is: 1616
FOS is: 84
The percent error is: 0.038
Parameters:
• 10ft long steel tube
• 1-1/2” square
• 0.120” wall
• A513 steel
False Position Method using Matlab:function [] = Buckling_False_Position()%Buckling_False_Position finds the value of max applicable load, F, that %the beam may support before collapse. %Calculate tube weight:dens=2.581; %slug/ft^3 http://www.clearpvcpipe.com/pdf/ClearPVCspecs.pdf OD=8.625/12; %OD of pipe in ft (SEE BOM)ID=7.943/12; %ID of pipe in ft (SEE BOM)L=15; %Length of pipe in ftV=(pi()/4)*(OD^2-ID^2)*L; %Volume of pipe in ft^3W=dens*V*32.2; %weight of the pipe in lbfWap=W/4; %weight at each connection point, assuming it's distributed %evenly across two bars with 2 connection points on eact bar %Calculate Pcra=1.5/12; %assuming a square x-section, the width in ftt=.12/12; %thickness of wall in ftb=a-2*t; %inner distace between wallsA=(a*a)-(b*b);l=10; %length in buckling in ftSyc=63100*(12^2); %Yield strength of A513 in lb/ft^3 (MATWEB)E=29700000*(12^2); %Elastic modulus of A513 in lb/ft^3 (MATWEB)e=OD/2+a/2+1/12; %eccentric distance, 1/2 of steel thickness + 1/2 OD of %vacuum tube + distance between edge of steel and vacuum tube c=a/2; %1/2 the distance across the cross-section of the hollow square barI=(1/12)*a*a^3-(1/12)*b*b^3; %Inertia of the bark=sqrt(I/A); %radius of gyrationf=@(F) F/A-Syc/(1+(e*c/k^2)*sec((l/(2*k))*sqrt(F/(A*E))));Fl=1;Fu=10000;Fn=Fu-f(Fu)*(Fu-Fl)/(f(Fu)-f(Fl));ed=.05;ea=100;iter=0;imax=100;while ea>ed && iter<imaxif f(Fl)*f(Fn)<0;Ft=Fn;Fu=Fn;elseif (f(Fl)*f(Fn))>0;Ft=Fn;Fl=Fn;enditer=iter+1;Fn=Fu-f(Fu)*(Fu-Fl)/(f(Fu)-f(Fl));ea=(abs((Fn-Ft)/(Fn)))*100;endFr=Fn;FOS=Fr/Wap;%ezplot(f,[1200,2000]); grid minor;fprintf('\n F (lbf) is: %.0f \n FOS is: %.0f \n The percent error is: %.3f \n',Fr,FOS,ea);end
Solution:
>> Buckling_False_Position
F (lbf) is: 1617
FOS is: 84
The percent error is: 0.006
Parameters:
• 10ft long steel tube
• 1-1/2” square
• 0.120” wall
• A513 steel
Graphical Method using Matlab:>> ezplot(f,[1200,2000]); grid minor;
1200 1300 1400 1500 1600 1700 1800 1900 2000
-1.5
-1
-0.5
0
0.5
1
1.5
x 105
F
F/A-Syc/(1+(e c/k2) sec((l/(2 k)) sqrt(F/(A E))))
Support Buckling Results
• We achieve a FOS well over what we would ever need for the selected support frame in buckling under worst case scenario
• Our frame can support the weight of the tube, and is feasible
• We can, if desired, reduce frame cross-section size and thickness if further analyses show large FOS as well
Engineering Analysis – StructureLeg Center Deflection
Worst case scenario:15’ Long PVC Schedule 408” Diameter10’ long square A513 tube1-1/2”
0.120” wall
A513 steel
Assumptions:Weight of vacuum is halved
between the two legs, as is the upper frame structure
1 foot long leg
Schematic
Reactions and DeflectionIn the diagram below, dimension a is the
distance to the front support block and b is to the center of the wheel axel.
F includes half the weight of the tube and the upper support structureResult: ymax=-3.30E-04
inches
Engineering Analysis SummaryProposed Requirement Metrics
Tower height: up to 5 meters (~16ft)Tower size: 6” DiameterNumber of Towers: 1Pump Speed: 6.25 cfm Pump Type: 2 stage Rotary (mechanical roughing
pump)Evacuation Time: 5.25 mins Ultimate Pressure: 15 microns (0.015Torr or 2Pa)Negative (Critical) Pressure – Factor of Safety: 3.94No Isolation Valves Manual Object LiftingElectromagnetic Release MechanismMobile Support Structure
Risk AssessmentID Risk Item Effect Cause
Likelihood
Severity
Importance
Action to Minimize Risk
1
Pipe Implodes
under Pressure
• Safety Hazard
• Project ruined
• Pipe wall thickness
• Material1 3 3
a) Determine critical pressure of pipe, with safety factor
2 Damages to pipe
• Loss of visibility
• Loss of Vacuum
• Shipping• Human
Error2 2 4
a) Careful shipment and assembly
b) Pick location where pipe is safe from accidental damages
c) Determine pipe resistances to scratches, crack, etc.
3 Pump Over heat
• Loss of efficiency
• Fire hazard• Pump
replacement
• Improper pump size
• Poorly ventilated
• Left on
1 2 2
a) Adequate space around pump for ventilation
b) Turn pump off when not in use
c) Limit the number of consecutive runs if needed
d) Analyze pump specifications
4 Tower Falls Over
• Safety Hazard
• Damages to Surroundings
• Project Ruined
• Poorly supported
• Earthquake• Weak
structure
1 3 3
a) Ensure tower can withstand its own weight
b) Develop sturdy designc) Attach tower to surrounding
wall, railings, etc. at different heights
ID
Risk Item Effect Cause L S I Action to Minimize
Risk
5Any
sealing leak
• Loss of Vacuum• Noisy• Increased
depressurize time
• Bad Sealant• Gaps in o-
rings• Surface
impurities
3 2 6
a) Require minimal seal pointsb) Research proper sealing
techniques for each component
c) Monitor pressure change
6Object Impact
breaks Base
• Object destroyed• Safety hazard• Pipe base broken• Loss of vacuum
• Cannot support objects force
1 2 2
a) Determine maximum force on impact (including safety factor)
b) Properly correct for that force with cushion, net, etc.
7
Laser Sensor Looses item
• Loss of data(position and time)
• Improper sensor alignment
• Sensor range inadequate
• Power loss
2 2 4
a) Determine whether vertical position sensor can detect all objects
b) Properly align sensor(s) with object
c) Ensure pipe connection can withstand that force
8Inaccurate
Gauge Reading
• Improper data display
• Improper vacuum
• Cheap gages• Not calibrated
correctly1 1 1
a) Calibrate all gage regularly (note in manual)
b) Purchase accurate & Reliable gages (tolerance)
9 Stolen components • Device unusable
• Components left out/unlocked
1 2 2
a) Bring components out when needed
b) Lock components up when not in use (near or away from tower)
ID Risk Item Effect Cause L S I Action to Minimize
Risk
10 Loss of Data
• Cant calculate gravity, drag and other data
• Loss of power• Software
malfunction1 2 2
a) Ensure Proper Electrical Connections
b) Capture all required datac) Possible sore multiple
run data
11Unsuccessful Release of objects
• Items does not fall
• Horizontal motion occurs
• Unsynchronized release
• Mechanism doesn’t open
• Release timing off
• Loss of power
2 2 4
a) Release objects simultaneously
b) Platform adequately centers objects
c) Robust latching mechanism
12Lifting device
Malfunction
• Item does not lift
• No dropping experiment
• Broken wire/ claw
• Loss of power• Improper motor
power
2 2 4
a) No lifting device, load form top
b) Ability to easily hold weight & size of objects
c) Ensure wire/cable does not get stuck
13Improper
use of system
• Compromises system integrity
• Poorly written manual
• Complicated operation
• Unauthorized use
1 1 1
a) Create intuitive design b) Create detailed
operators manualc) Limit use to qualified
individuals
Test Plan# Test Description Comments/Status
1 Energy Dissipation Control Drop heaviest object
2 Test Release Mechanism Drop Object from any height
3 Position sensor accuracy for objects Sensors can be mounted / tested without tube
4 Ultimate pressure Considering pump size / leaks/ chamber volume
5 Pressure gage accuracy Connect vacuum to pressure gage only
6 Temperature gage accuracy Calibrate Sensor
7 DAQ device inputs Position and time (from sensor(s))
8 Computer Software Outputs Computer outputs from on DAQ & human inputs
9 Tower stability Simulate maximum applied forces
10 Extra vacuum tests How things react inside our vacuum
MSD I Project ScheduleAug September October November December1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18
Planning & Execution
Problem Definition
System Design
Subsystem Design
Detailed Design
Address Open Issues
Complete Release Mechanism Design
Schedule PDR and Invite Participants
Update Test Plan
Update Edge
Finalize Support Structure
Complete Drawing Package
Finalize Bill of Material
Finalize Continuous Lift Concepts
Bill of Materials
Questions?