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CORNELL ROCKETRYTEAM
Design Portfolio
Matthew Gentile
Cornell University
M.Eng. in Aerospace Structures: December 2015
B.S. in Mechanical and Aerospace Engineering
Matthew Gentile
Design Portfolio
Jet Propulsion Laboratory Co-op Fall 2013
Low Density Super Sonic Decelerators (LDSD)
• One of three heat shield mini-pallet assemblies
for LDSD water recovery aids
• Aluminum andTeflon construction for heat
resistance and RF transparency
• Model and GD&T drawings created in NX Unigraphics
Matthew Gentile
Design Portfolio
Jet Propulsion Laboratory Co-op Fall 2014
Europa Clipper Project
• 1:16 scale Solar Europa Clipper
spacecraft
• 3D printed: FDM multicolored
ABS for each module
• Created in NX Unigraphics
• Assembled by a series of pins and magnets
• Both stowed and deployed solar panels
• Worked on mass properties for the
Pre-Phase A Europa Clipper configuration
Matthew Gentile
Design Portfolio
Jet Propulsion Laboratory Co-op Fall 2014
Europa Clipper Project
 3D printed 6:1 scale radiation vault for Solar Europa Clipper configuration
 Magnets allow panels to be removed for easy viewing
 Clear SLA material
Matthew Gentile
Design Portfolio
MAE 2250: Mechanical Synthesis MAE 3780: Mechatronics
• Wind powered water pump capable of 11 L/min
• Aluminum, steel, and PVC construction
• Manufactured on a manual mill and lathe
• Model and drawings created in Solidworks
• Sumobot for mechatronics
competition
• Programmed in C
• Finished 4th out of 60 teams
Matthew Gentile
Design Portfolio
Cornell RocketryTeam (CRT): Vice President 2011-2012
Clifford: First Full Carbon Fiber Composite Airframe
• Unidirectional carbon fiber
core for tail-to-tip strength
• Biaxial carbon fiber shell for
impact resistance
• Two flights to 1,500 ft and
5,600 ft in PennYan, NY
Matthew Gentile
Design Portfolio
Cornell RocketryTeam (CRT): Vice President 2013-2014
Darth Maul: Carbon and Fiberglass Reinforced Phenolic Airframe
• First large dual deploy launch vehicle
• 11.5 feet tall, 6 inches in diameter
• Launched in PennYan, NY as a test rocket for the 2013-2014 NASA SL
Matthew Gentile
Design Portfolio
Cornell RocketryTeam (CRT)Vice President 2013-2014
HADIS: High Altitude Dual In-Line Staging – Fiberglass Reinforced Airframe
• 76 inches tall, 2.56 inches in diameter
• Two-stage dual deploy launch vehicle
• Reached an apogee of 2,500 ft
• Parachutes made in-house
Matthew Gentile
Design Portfolio
Cornell RocketryTeam (CRT)Vice President 2013-2014
HADIS: High Altitude Dual In-Line Staging
• First launch to 2,500 ft in Price, MD
• Full-scale Solidworks model for
2013-2014 NASA SL CDR
Matthew Gentile
Design Portfolio
Cornell RocketryTeam (CRT) President 2014-2015
2014-2015 NASA SL Competition
Senior Design Project: Gravity Assist Launch Pad
• Preliminary Solidworks design of gravity assist launch pad
• Actuates from horizontal to vertical via a counter weight, rotational
damper, and burn wire separation mechanism
• CDR design and fabrication will be completed by February 2015
Matthew Gentile
Design Portfolio
Cornell RocketryTeam (CRT) President 2014-2015
2014-2015 NASA SL
Subscale LaunchVehicle
• Three events: drogue deploy at apogee, payload deploy at 1,000 ft,
and main deploy at 700 ft. Reached an apogee of 3,270 ft
• 74 inches tall, 4 inches in diameter
• On board HD video from payload section

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Design Portfolio 122814

  • 1. CORNELL ROCKETRYTEAM Design Portfolio Matthew Gentile Cornell University M.Eng. in Aerospace Structures: December 2015 B.S. in Mechanical and Aerospace Engineering
  • 2. Matthew Gentile Design Portfolio Jet Propulsion Laboratory Co-op Fall 2013 Low Density Super Sonic Decelerators (LDSD) • One of three heat shield mini-pallet assemblies for LDSD water recovery aids • Aluminum andTeflon construction for heat resistance and RF transparency • Model and GD&T drawings created in NX Unigraphics
  • 3. Matthew Gentile Design Portfolio Jet Propulsion Laboratory Co-op Fall 2014 Europa Clipper Project • 1:16 scale Solar Europa Clipper spacecraft • 3D printed: FDM multicolored ABS for each module • Created in NX Unigraphics • Assembled by a series of pins and magnets • Both stowed and deployed solar panels • Worked on mass properties for the Pre-Phase A Europa Clipper configuration
  • 4. Matthew Gentile Design Portfolio Jet Propulsion Laboratory Co-op Fall 2014 Europa Clipper Project  3D printed 6:1 scale radiation vault for Solar Europa Clipper configuration  Magnets allow panels to be removed for easy viewing  Clear SLA material
  • 5. Matthew Gentile Design Portfolio MAE 2250: Mechanical Synthesis MAE 3780: Mechatronics • Wind powered water pump capable of 11 L/min • Aluminum, steel, and PVC construction • Manufactured on a manual mill and lathe • Model and drawings created in Solidworks • Sumobot for mechatronics competition • Programmed in C • Finished 4th out of 60 teams
  • 6. Matthew Gentile Design Portfolio Cornell RocketryTeam (CRT): Vice President 2011-2012 Clifford: First Full Carbon Fiber Composite Airframe • Unidirectional carbon fiber core for tail-to-tip strength • Biaxial carbon fiber shell for impact resistance • Two flights to 1,500 ft and 5,600 ft in PennYan, NY
  • 7. Matthew Gentile Design Portfolio Cornell RocketryTeam (CRT): Vice President 2013-2014 Darth Maul: Carbon and Fiberglass Reinforced Phenolic Airframe • First large dual deploy launch vehicle • 11.5 feet tall, 6 inches in diameter • Launched in PennYan, NY as a test rocket for the 2013-2014 NASA SL
  • 8. Matthew Gentile Design Portfolio Cornell RocketryTeam (CRT)Vice President 2013-2014 HADIS: High Altitude Dual In-Line Staging – Fiberglass Reinforced Airframe • 76 inches tall, 2.56 inches in diameter • Two-stage dual deploy launch vehicle • Reached an apogee of 2,500 ft • Parachutes made in-house
  • 9. Matthew Gentile Design Portfolio Cornell RocketryTeam (CRT)Vice President 2013-2014 HADIS: High Altitude Dual In-Line Staging • First launch to 2,500 ft in Price, MD • Full-scale Solidworks model for 2013-2014 NASA SL CDR
  • 10. Matthew Gentile Design Portfolio Cornell RocketryTeam (CRT) President 2014-2015 2014-2015 NASA SL Competition Senior Design Project: Gravity Assist Launch Pad • Preliminary Solidworks design of gravity assist launch pad • Actuates from horizontal to vertical via a counter weight, rotational damper, and burn wire separation mechanism • CDR design and fabrication will be completed by February 2015
  • 11. Matthew Gentile Design Portfolio Cornell RocketryTeam (CRT) President 2014-2015 2014-2015 NASA SL Subscale LaunchVehicle • Three events: drogue deploy at apogee, payload deploy at 1,000 ft, and main deploy at 700 ft. Reached an apogee of 3,270 ft • 74 inches tall, 4 inches in diameter • On board HD video from payload section