Notes
Slide Show
Outline
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Hey Bubba, Watch This!
Level 3 Certification Package
  • Chuck Pierce
  • TRA 9308
  • NAR 78629


  • Southern Thunder Launch
  • Manchester, TN
  • June 3, 2006


  • TAPs:  Walt Stafford, Tom Binford
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Overview
  • The objective of this package is to discuss the design, configuration, and test history of Hey Bubba.
    • Rocket Overview
    • Aft Airframe (including motor mount) Construction
    • Forward Airframe Construction
    • Nose Cone Construction
    • Avionics Bay Construction and Function
    • Recovery System Construction and Function
    • Rocket Attributes
    • Flight Predictions
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Rocket Overview
  • Construction
    • Hey Bubba has been constructed from
    •     Performance Rocketry components
      • Two 6” dia x 48” long Fiberglass airframe tubes
      • Fiberglass Fincan
      • 5:1 Ogive Fiberglass nose cone
    • Bulkheads and Centering Rings are handmade from ¾” Plywood
  • Final Specifications
    • Mass (no motor): 28 lbs
    • Mass (with M1350): 40 lbs
    • Final Mass: 33 lbs
  • Stability
    • Hey Bubba has been verified to have 2.5 to 3.0 calibers of stability, based on Barrowman and RockSim CP calculations, respectively
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Aft Airframe Construction
  • Airframe:
    • Performance Rocketry 6” OD, 1/8” Wall, 48” long Fiberglass Tubing
  • Motor Mount Assembly
    • Motor Tube
      • 3” ID x 1.8” wall x 31” long paper tube
      • 4 Plywood Centering Rings, ¾” thick
        • Epoxied to motor tube and airframe ID
        • Forward-most and two aft-most CRs are also attached to airframe with three #8-32 CRES machine screws
        • Aft-most CR is chamfered
          • ½” is same OD as airframe and is external to Airframe
          • ¼” is same ID as airframe and is internal to the Airframe
          • Purpose of chamfer:  To allow the aft CR to apply the thrust force directly into the long axis of the airframe, thus helping to avoid a shear failure of the MMT inside the airframe.
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Aft Airframe Construction (Cont)
  • Forward Bulkhead
    • ¾” Plywood
    • Attachment to Airframe
      • Epoxied to ID
      • Three #8-32 machine screws through Airframe into bulkhead
    • Motor Retention
      • 3/8” hole in bulkhead
      • 3/8” x 6” threaded rod screws into Motor bulkhead.  Washer and wingnut attaches motor and retention rod to bulkhead
    • Drogue Parachute Harness Attachment
      • 5/16” U-Bolt permanently attached to bulkhead
      • Offset off airframe centerline to allow access to retention rod
    • Volume of Drogue Chute Compartment is 424 in3
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Aft Airframe Construction (Cont)
  • Fin Set
    • Single-piece Performance Rocketry Fiberglass 3-fin Fin Can
    • Flush with aft side of Aft CR (½” aft of airframe tubing)
    • Epoxied to OD of Airframe
    • Mechanically attached with six #8-32 CRES screws
      • 3 each into two aft-most Centering Rings
  • Rail Guides
    • Rail Guides are screwed into aft-most and forward-most Centering Rings with #8-32 screws
      • Nylon insert allows Large Rail Buttons to be securely attached
      • May also use Small Rail Buttons, if desired, for future flights.
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Aft Airframe Construction (Cont)
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FWD Airframe Construction
  • Airframe:
    • Performance Rocketry 6” OD, 1/8” Wall, 48” long Fiberglass Tubing
  • Coupler
    • Performance Rocketry Fiberglass Coupler, 12” Long
    • 6” permanently attached in Airframe
      • Epoxied into ID of Airframe
      • Six #8-32 screws run through Aiframe and Coupler and into bulkhead (3 screws attach to two bulkheads
    • ¾” Plywood Bulkhead terminates aft end of Coupler
      • 5/16” U-bolt permanently attached to bulkhead
      • Drogue Ejection Charge Terminal Blocks permanently attached to bulkhead
      • Bulkhead epoxied into ID of Coupler.  Three #8-32 set screws further secures bulkhead
    • Avionics Bay enclosed in forward end of Coupler
  • Forward Bulkhead (¾” Plywood)
    • Attachment to Airframe
      • Epoxied to ID
      • Three #8-32 machine screws through Airframe into bulkhead
    • Main Parachute Harness Attachment
      • 5/16” U-Bolt permanently attached to bulkhead
      • Offset off airframe centerline to allow access to retention rod
    • Main Ejection Charge Terminal Blocks permanently attached to bulkhead
  • Volume of Main Chute Compartment is 707 in3
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FWD Airframe Construction (Cont)
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Nose Cone Construction
  • Performance Rocketry Fiberglass Nose
    • 5:1 (eg, 30”) ogive
    • 6” long shoulder
  • ¾” Plywood Bulkhead terminates aft end of Coupler
      • 5/16” U-bolt permanently attached to bulkhead
      • Bulkhead epoxied into ID of Shoulder.
      • Three #8-32 set screws further secures bulkhead
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Avionics Bay Construction & Function
  • Construction
    • Internal ¾” Plywood Bulkhead located flush with aft end of airframe. Closes aft end of Avionics Bay
    • Internal ¼” plywood bulkhead closes forward end of Avionics Bay
    • Side Entry allows easy access into the Avionics Bay
    • Two switches with external, removable keys
    • ¼” plywood sled holds two altimeters
    • Plywood races guide altimeter sled into place and securely hold altimeters in place during flight.
    • Volume of Altimeter Bay is 142 in3
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Avionics Bay Construction and Function (Cont)
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Avionics Bay Construction and Function (Cont)
  • Function
    • Configuration
      • Fully Redundant Altimeter System
        • Dual PF MAWD altimeters
        • Dedicated Key Switch for each altimeter
        • Dedicated battery pack for each altimeter
        • Dedicated Drogue charge wires and Main charge wires for each altimeter
      • Altimeter Settings
        • Mach Delay: 8 seconds
        • Drogue Charge: Apogee
        • Main Charge: 700 feet
    • Testing
      • MAWD Altimeters each tested in homemade altitude chamber
        • Verified apogee and proper drogue and main charge function
      • Drogue and Main Parachute Ejection Charges fully tested in flight configuration
        • Verified strong ejection (~10’ of separation, parachutes fully ejected from airframe)
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Recovery System Construction & Function
  • Drogue Parachute System
    • Drogue Parachute:  B2 Rocketry Cert-3 Drogue (~24” dia)
    • Drogue Harness: 5/8” tubular Kevlar, 60’ long
    • 3/8” Quick Link at each end
    • Drogue Parachute attached 10’ from forward end of Drogue Harness
    • RocketHunter Transmitter electrical-taped to Drogue Harness
    • Drogue Compartment Volume:  424 in3
    • Drogue Compartment held closed with 4 x #2-56 nylon screws
    • Drogue Ejection Charge:  2.75 grams
      • Generates 12.6 psi for an Ejection Force of 356 lbf
      • Successfully ground tested on 5/28/2006 in flight configuration
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Recovery System Construction & Function
  • Main Parachute System
    • Main Parachute:  Rocketman R14C
    • Drogue Harness: 5/8” tubular Kevlar, 30’ long
    • 3/8” Quick Link at each end
    • Main Parachute attached 10’ from forward end of Drogue Harness
    • Main Chute Compartment Volume:  707 in3
    • Main Compartment held closed with 4 x #2-56 nylon screws
    • Drogue Ejection Charge:  5.5 grams
      • Generates 15.1 psi for an Ejection Force of 427 lbf
      • Successfully ground tested on 5/27/2006 in flight configuration
    • Main Chute deployed at 700’
    • Velocity at landing:  20 fps

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Rocket Attributes
  • Gross Liftoff Weight:  40 lbm
  • Landing Weight:    33 lbm
  • Stability (Calculated using RockSim 7.0)
    • CP Location:
      • 17.5” from base (RockSim Equation)
      • 21.5” from base (Barrowman Equation)
    • CG Location
      • 39” from base (hand measured in flight configuration)
    • Stability Margin
      • 3 calibers (Barrowman CP)
      • 3.6 calibers (RockSim CP)

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Flight Predictions
  • Predictions performed using RockSim 7.0
  • Rocket Attributes
    • GLOW (w/ motor): 40 lbs
    • Landing Weight: 33 lbs
    • Motor:  AMW M1350
      • Max Thrust: 1662N (373 lbf)
  • Launch
    • 44 fps achieved in 46” of travel
    • Thrust/Weight: 9.3
  • Main Deployment
    • Altitude:  700’ (pre-set)
    • Velocity at deployment: 101 fps
  • Landing
    • Velocity: 20 fps
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Concluding Remarks
  • Excellent Structural Integrity
    • Performance Rocketry Airframe, Fincan, Nosecone, Coupler
    • Handmade Centering Rings and Bulkheads from ¾” Plywood
    • CRs attached to Motor tube with 30-min epoxy, w/ generous fillets
    • CRs and Bulkheads attached inside FG Airframe and Coupler with 30-min epoxy and 3 #8-32 screws (each).
    • FG Fincan attached to FG Airframe w/ 30-min epoxy and six #8-32 screws.
    • Motor retained by 3/8” threaded rod in forward closure
  • Ample Stability Margin (at least 3 calibers in launch configuration)
  • Robust Recovery System
    • Fully Redundant Electronics
      • Each of two altimeters has dedicated key switch, battery pack, drogue charge, main charge
      • Both altimeters are PF MAWDs, which has high reliability
      • Both altimeters have been individually tested in homemade altitude chamber
    • Ejection Charges have been fully tested and provide excellent ejection force and approximately 10’ of separation during ground test and parachutes fully ejected from airframe.
    • B2Rocketry Cert-3 Drogue Chute
    • Rocketman R14C Main Chute
    • Tubular Kevlar Harnesses (60’ for Drogue, 30’ for Main)
    • 101 fps Drogue Descent Velocity is acceptable
    • 20 fps Landing Velocity is acceptable for Manchester Field
    • RocketHunter xmitter attached to Drogue Harness
  • Good Motor for Hey Bubba
    • 9.3 Thrust/Weight
    • 8600 feet, predicted altitude
  • Biggest Concern for this flight?
    • Staying out of the trees!