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3D-Printed Hybrid Rocket Fuel Grains
Fused Layer ABS Rocketry Experiment
(F.L.A.R.E)
Amy Besio
Jonathan Benson
Richard Horta
John Seligson
Josh Rou
Faculty/Technical
Advisor:
Justin Karl, Ph.D.
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Amy Besio – Project Manager/Propulsion System Design 1
• Mission Statement
• To design, fabricate, and test 3D-printed fuel
grains to optimize hybrid rocket performance
characteristics
• Hybrid Rockets
• Safer
• Non-toxic/non-explosive
propellants
• Command shutdown and
throttling capabilities
• Ease of transport, storage,
and handling
Design Objectives
Liquid
Oxidizer
Igniter
Injector
Solid Fuel
Grain
Nozzle
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Amy Besio – Project Manager/Propulsion System Design 2
Ground Test Article
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Josh Rou – Oxidizer Feed System 3
Design Problem
• Hybrid Rocket Disadvantages
• Lower performance
• Low regression rate
• Mass Flow Rate
• Oxidizer
• Valve Size Dependent
• Fuel
• Surface Area Dependent
• Complex Thrust Profile
• Needs Complex Grain Geometries
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Josh Rou – Oxidizer Feed System 4
Our Solution
• Optimize exposure of fuel grain
surface area through 3D printing
• Advantages of 3D printing
• Precision
• Relatively Inexpensive
• Readily Available
• Comparable performance
characteristics to HTPB
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Josh Rou – Oxidizer Feed System 5
Three Parallel Development Projects
• Test Stand
• Ground Test Article
• Flight Vehicle - End Goal
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Richard Horta – Test Stand Design 6
Testing System
• Preliminary Design Requirements
• Factor of Safety = 5
• Cost Effectiveness
• Ease of Maintenance
• Portability
• Compatibility
• Previous Designs
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Richard Horta – Test Stand Design 7
Testing System
• Rails Angled 45 Degrees
• Superstrut Platform and Clamps
• Fabrication
• Cutting, Grinding, Deburring
• Milling
• Drilling
• Welding
• Coating
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Jonathan Benson – Data Acquisition 8
• Instrumentation Integration
• Button Load Cell
• 12 Volt Excitation
• Pressure Transducers
• 5 Volt Excitation
• External Instrument
• IR Meter
Testing System
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Jonathan Benson – Data Acquisition 9
Testing System - Results & Performance
• Pressure Experienced in Testing
• Oxidizer Pressure 4480 kPa
• Combustion Chamber Pressure
4000 kPa
• Temperature Experienced in Testing
• 578 Kelvin
• Force Experienced in Testing
• 1500 Newtons
• Test Stand Performance
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Amy Besio – Project Manager/Propulsion System Design 10
Ground Test Article
• Design Requirements
• Oxidizer/Fuel
• N2O/ABS
• ID: 54 mm
• Force: 500-1000 N
• Chamber Pressure: 3.45 MPa
• Factor of Safety: 2x
• Design Outputs
• Thrust
• Mass Flow Rate
• Chamber Pressure
• Exit Temperature
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Amy Besio – Project Manager/Propulsion System Design
Ground Test Article
• Design Considerations
• Thermochemical Evaluation
• N2O/ABS
• 7.8:1
• Combustion Temperature: 3500 K
• Combustion Chamber
• 6061-T6 Aluminum
• 54 mm X 160 mm
• Nozzle
• Ideally expanded
• Pe=Pa
𝐴 𝑡
=
𝑚 𝑝
𝑃𝑡
𝑅 ∗ 𝑇𝑡
𝑘
= 95 𝑚𝑚2
𝑀𝑒 =
2
𝑘 − 1
∗
𝑃𝑐
𝑃𝑎
𝑘−1
2
− 1 = 2.96
𝐴 𝑒 =
𝐴 𝑡
𝑀𝑒
1 +
𝑘 − 1
2
𝑀𝑒
2
𝑘 + 1
2
𝑘+1
2 𝑘−1
= 490 𝑚𝑚2
𝑉𝑒 =
2𝑘
𝑘−1
∗ 𝑅 ∗ 𝑇𝑐 ∗ 1 −
𝑃𝑒
𝑃𝑐
𝑘−1
𝑘
𝐹 = 𝑚 𝑝 𝑉𝑒 + 𝑃𝑒 − 𝑃𝑎 𝐴 𝑒
11
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Amy Besio – Project Manager/Propulsion System Design
Ground Test Article
• Expected Performance
• Mass Flow Rate
• 0.282 kg/s
• Force
• 670 N
• Specific Impulse
• 194 seconds
• Regression Rate
12
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Amy Besio – Project Manager/Propulsion System Design
Ground Test Article - Testing
Test 1: Live Fire Sequencing
(subsonic)
Test 2: Solid Fuel Pressure
Test
13
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Amy Besio – Project Manager/Propulsion System Design
Ground Test Article - Testing
14
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Amy Besio – Project Manager/Propulsion System Design
Rocket
-100
0
100
200
300
400
500
0 1 2 3 4 5
Force(N)
Time (s)
Thrust- Comparison
90% Infill 25% Infill
90% 25%
Mass Flow
Rate
155 g/s 152 g/s
Thrust 405 N 422 N
Combustion
Pressure
3.9 MPa 3.9 MPa
15
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
John Seligson – Data Acquisition
Flight Ready Model
• Type of Motor - Contrial J-245
• 2000m Expected Altitude
• 644 Ns Total Impulse
• 3 s Burn Time
• Flight Mechanics Design
Considerations
• Fins - CP Aft of CG
• Nose Cone - Rounded Curve
• Testing of Remaining Fuel Grains
• 90% Infill
• 25% Infill
• Variable Infill
[Peterson]
16
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
John Seligson – Data Acquisition
Flight Ready Vehicle
• Measurements/Control
• Altimetry
• Positioning
• Orientation
• Temperature
• Visual Recording
Component Make Model
Microcontroller PJRC Teensy++ 2.0
SD Adapter PJRC SD Adapter
Altimeter adafruit BMP180
GPS adafruit GPS Breakout
Gyroscope adafruit LSM9DSO
Thermocouple adafruit Type-K Glass Braid
Camera GoPro Hero
17
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Jonathan Benson – Data Acquisition
Recommendations
• Development
• Infill of 3D printers
• Different 3D printed Materials
• Nylon
• Polycarbonate
• Different Oxidizers
• Liquid Oxygen
• Design
• New Geometries
18
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Amy Besio – Project Manager/Propulsion System Design 19
Budget
System Previous Current
Test Stand Structure $450.00 $100.00
Data Acquisition Equipment $500.00 $200.00
Rocket Components $650.00 $425.00
Propellant $200.00 $605.00
Total $1800.00 $1330.00
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Amy Besio – Project Manager/Propulsion System Design
Acknowledgements
20
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Questions?
21
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Alternate Slide - Test Stand Assembly
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Alternate Slide - Test Stand Assembly
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Alternate Slide - Oxidizer Feed System
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Alternate Slide - Oxidizer Feed System
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Alternate Slide - Oxidizer Feed System
Pressure Relief Valves Solenoid Valves
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Alternate Slide - Oxidizer Feed System
Trial
Number
Scale
Precision
(g)
Solenoid Valve
Orifice Diameter
(cm)
∆Mass
(g)
∆Time
(seconds)
Mass
Flow Rate
(g/s)
Component
Removed
Component
Added
Trial 1 50 0.196 100 2.27 44 - -
Trial 2 50 0.196 300 5.33 56 CV -
Trial 3 50 0.196 300 4.99 60 CV, Tubing, ⅛”
Right-Angle
Adapters
-
Trial 4 2 0.196 276 5.24 52.67 CV -
Trial 5 2 0.196 108 1.94 55.67 CV -
Trial 6 2 0.196 102 1.85 55.14 CV -
Trial 7 2 0.635 464 1.93 240.41 CV Large SV, (2)
¼”Tee Adapters
Trial 8 2 0.635 424 1.91 221.99 CV Large SV, (2)
¼”Tee Adapters
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Alternate Slide - Thermal Imaging
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Alternate Slide - Data Acquisition
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Alternate Slide - Data Acquisition
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Alternate Slide - Data Acquisition
University of Central Florida-Senior Design Fall 2015
3D Printed Hybrid Rocket Fuel Grains
Alternate Slide - Data Acquisition

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FLARE_Final_Presentation

  • 1. 3D-Printed Hybrid Rocket Fuel Grains Fused Layer ABS Rocketry Experiment (F.L.A.R.E) Amy Besio Jonathan Benson Richard Horta John Seligson Josh Rou Faculty/Technical Advisor: Justin Karl, Ph.D.
  • 2. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Amy Besio – Project Manager/Propulsion System Design 1 • Mission Statement • To design, fabricate, and test 3D-printed fuel grains to optimize hybrid rocket performance characteristics • Hybrid Rockets • Safer • Non-toxic/non-explosive propellants • Command shutdown and throttling capabilities • Ease of transport, storage, and handling Design Objectives Liquid Oxidizer Igniter Injector Solid Fuel Grain Nozzle
  • 3. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Amy Besio – Project Manager/Propulsion System Design 2 Ground Test Article
  • 4. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Josh Rou – Oxidizer Feed System 3 Design Problem • Hybrid Rocket Disadvantages • Lower performance • Low regression rate • Mass Flow Rate • Oxidizer • Valve Size Dependent • Fuel • Surface Area Dependent • Complex Thrust Profile • Needs Complex Grain Geometries
  • 5. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Josh Rou – Oxidizer Feed System 4 Our Solution • Optimize exposure of fuel grain surface area through 3D printing • Advantages of 3D printing • Precision • Relatively Inexpensive • Readily Available • Comparable performance characteristics to HTPB
  • 6. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Josh Rou – Oxidizer Feed System 5 Three Parallel Development Projects • Test Stand • Ground Test Article • Flight Vehicle - End Goal
  • 7. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Richard Horta – Test Stand Design 6 Testing System • Preliminary Design Requirements • Factor of Safety = 5 • Cost Effectiveness • Ease of Maintenance • Portability • Compatibility • Previous Designs
  • 8. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Richard Horta – Test Stand Design 7 Testing System • Rails Angled 45 Degrees • Superstrut Platform and Clamps • Fabrication • Cutting, Grinding, Deburring • Milling • Drilling • Welding • Coating
  • 9. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Jonathan Benson – Data Acquisition 8 • Instrumentation Integration • Button Load Cell • 12 Volt Excitation • Pressure Transducers • 5 Volt Excitation • External Instrument • IR Meter Testing System
  • 10. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Jonathan Benson – Data Acquisition 9 Testing System - Results & Performance • Pressure Experienced in Testing • Oxidizer Pressure 4480 kPa • Combustion Chamber Pressure 4000 kPa • Temperature Experienced in Testing • 578 Kelvin • Force Experienced in Testing • 1500 Newtons • Test Stand Performance
  • 11. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Amy Besio – Project Manager/Propulsion System Design 10 Ground Test Article • Design Requirements • Oxidizer/Fuel • N2O/ABS • ID: 54 mm • Force: 500-1000 N • Chamber Pressure: 3.45 MPa • Factor of Safety: 2x • Design Outputs • Thrust • Mass Flow Rate • Chamber Pressure • Exit Temperature
  • 12. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Amy Besio – Project Manager/Propulsion System Design Ground Test Article • Design Considerations • Thermochemical Evaluation • N2O/ABS • 7.8:1 • Combustion Temperature: 3500 K • Combustion Chamber • 6061-T6 Aluminum • 54 mm X 160 mm • Nozzle • Ideally expanded • Pe=Pa 𝐴 𝑡 = 𝑚 𝑝 𝑃𝑡 𝑅 ∗ 𝑇𝑡 𝑘 = 95 𝑚𝑚2 𝑀𝑒 = 2 𝑘 − 1 ∗ 𝑃𝑐 𝑃𝑎 𝑘−1 2 − 1 = 2.96 𝐴 𝑒 = 𝐴 𝑡 𝑀𝑒 1 + 𝑘 − 1 2 𝑀𝑒 2 𝑘 + 1 2 𝑘+1 2 𝑘−1 = 490 𝑚𝑚2 𝑉𝑒 = 2𝑘 𝑘−1 ∗ 𝑅 ∗ 𝑇𝑐 ∗ 1 − 𝑃𝑒 𝑃𝑐 𝑘−1 𝑘 𝐹 = 𝑚 𝑝 𝑉𝑒 + 𝑃𝑒 − 𝑃𝑎 𝐴 𝑒 11
  • 13. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Amy Besio – Project Manager/Propulsion System Design Ground Test Article • Expected Performance • Mass Flow Rate • 0.282 kg/s • Force • 670 N • Specific Impulse • 194 seconds • Regression Rate 12
  • 14. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Amy Besio – Project Manager/Propulsion System Design Ground Test Article - Testing Test 1: Live Fire Sequencing (subsonic) Test 2: Solid Fuel Pressure Test 13
  • 15. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Amy Besio – Project Manager/Propulsion System Design Ground Test Article - Testing 14
  • 16. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Amy Besio – Project Manager/Propulsion System Design Rocket -100 0 100 200 300 400 500 0 1 2 3 4 5 Force(N) Time (s) Thrust- Comparison 90% Infill 25% Infill 90% 25% Mass Flow Rate 155 g/s 152 g/s Thrust 405 N 422 N Combustion Pressure 3.9 MPa 3.9 MPa 15
  • 17. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains John Seligson – Data Acquisition Flight Ready Model • Type of Motor - Contrial J-245 • 2000m Expected Altitude • 644 Ns Total Impulse • 3 s Burn Time • Flight Mechanics Design Considerations • Fins - CP Aft of CG • Nose Cone - Rounded Curve • Testing of Remaining Fuel Grains • 90% Infill • 25% Infill • Variable Infill [Peterson] 16
  • 18. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains John Seligson – Data Acquisition Flight Ready Vehicle • Measurements/Control • Altimetry • Positioning • Orientation • Temperature • Visual Recording Component Make Model Microcontroller PJRC Teensy++ 2.0 SD Adapter PJRC SD Adapter Altimeter adafruit BMP180 GPS adafruit GPS Breakout Gyroscope adafruit LSM9DSO Thermocouple adafruit Type-K Glass Braid Camera GoPro Hero 17
  • 19. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Jonathan Benson – Data Acquisition Recommendations • Development • Infill of 3D printers • Different 3D printed Materials • Nylon • Polycarbonate • Different Oxidizers • Liquid Oxygen • Design • New Geometries 18
  • 20. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Amy Besio – Project Manager/Propulsion System Design 19 Budget System Previous Current Test Stand Structure $450.00 $100.00 Data Acquisition Equipment $500.00 $200.00 Rocket Components $650.00 $425.00 Propellant $200.00 $605.00 Total $1800.00 $1330.00
  • 21. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Amy Besio – Project Manager/Propulsion System Design Acknowledgements 20
  • 22. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Questions? 21
  • 23. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Alternate Slide - Test Stand Assembly
  • 24. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Alternate Slide - Test Stand Assembly
  • 25. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Alternate Slide - Oxidizer Feed System
  • 26. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Alternate Slide - Oxidizer Feed System
  • 27. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Alternate Slide - Oxidizer Feed System Pressure Relief Valves Solenoid Valves
  • 28. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Alternate Slide - Oxidizer Feed System Trial Number Scale Precision (g) Solenoid Valve Orifice Diameter (cm) ∆Mass (g) ∆Time (seconds) Mass Flow Rate (g/s) Component Removed Component Added Trial 1 50 0.196 100 2.27 44 - - Trial 2 50 0.196 300 5.33 56 CV - Trial 3 50 0.196 300 4.99 60 CV, Tubing, ⅛” Right-Angle Adapters - Trial 4 2 0.196 276 5.24 52.67 CV - Trial 5 2 0.196 108 1.94 55.67 CV - Trial 6 2 0.196 102 1.85 55.14 CV - Trial 7 2 0.635 464 1.93 240.41 CV Large SV, (2) ¼”Tee Adapters Trial 8 2 0.635 424 1.91 221.99 CV Large SV, (2) ¼”Tee Adapters
  • 29. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Alternate Slide - Thermal Imaging
  • 30. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Alternate Slide - Data Acquisition
  • 31. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Alternate Slide - Data Acquisition
  • 32. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Alternate Slide - Data Acquisition
  • 33. University of Central Florida-Senior Design Fall 2015 3D Printed Hybrid Rocket Fuel Grains Alternate Slide - Data Acquisition