Recovery Systems Tripoli Minnesota Gary Stroick December 2012.
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Transcript of Recovery Systems Tripoli Minnesota Gary Stroick December 2012.
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Recovery Systems
Tripoli MinnesotaGary Stroick
December 2012
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Copyright © 2012 by Off We Go Rocketry, LLC 2
Agenda
• Overview• Dual Deployment Designs• Avionics Bays• Electronics & Ejection• Attachment Points• Parachutes & Packing• Summary
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Overview
• Why use Dual Deployment?1. To stay out of mosquito infested
swamps.2. To reduce the drift distance ensuring
that the vehicle remains in the recovery area as specified by the Tripoli Safety Code.
3. So those with bad hips don’t have to walk so far.
Unless …
You’reBill
You’reVerno
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Overview
• Two Stage Recovery Philosophy• Initial Rapid Controlled Descent
• Descent Rate 100 ft/sec• Techniques: Flat Spin, Body Separation,
Streamer, Parachute
• Slow Final Descent• Descent Rate 20 ft/sec• Techniques: Parachute
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Failure Modes
Attachment Points• Quick Links not Connected
or Left Open• Poor Knot Selection• Inadequate Hardware
Deployment• Too Small/Not Tested• Incorrect Altimeter Setup• Loss of Power• Electrical Wire Disconnects
Parachute, Bridle, etc.• Improperly Folded• Improperly Sized• Inadequately Protected• Fatigue Considerations
Related Failures• Drag Separation• Zippers• In Flight Self Impact• Shear Pin Failure
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#1 Cause of Failure is Recovery!
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Dual Deployment Designs
• Design Approaches1. Split Airframe Deployment2. Inline Deployment3. Rear Deployment4. Hatch Deployment
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Split Airframe
Typical & Most Popular Design
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Booster Section
Drogue Chute
Airframe Splits
AV Bay Main Chute
Top of Airframe
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Split Airframe
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Ejection Charges
Ejection Charges
Avionics Bay
Rivets
AttachmentPoints
AttachmentPoints
(Bad!)MainBridle
DrogueBridle
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Inline
Typical Design
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AirframeDrogueEjectionCharge
PistonRetainer
Line
Main Chute
ARRD Wiring
AV BayCoupler
Main Bridle
Piston Support
RingPiston BridleARRDEye Bolt
Drogue Chute
Drogue BridlePiston
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Rear
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Parachute
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Hatch
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Avionics (AV) Bays
• Design Philosophies• Redundant Systems (if possible)• Complete System Independence
• Power• Switches
• Separate Power Sources• Altimeter• Pyro Channels
• Ease of Use!12Copyright © 2012 by Off We Go Rocketry, LLC
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AV Bay
Internal Components• Avionics Mount
• Usually a Sled• Z-Axis Alignment
• Internal Sled Support• Rods & Tube/Eyes• Slotted Bulkheads
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AV Bay
Power Systems• Batteries
• 9V Duracell or Werker (Soldered)• LiPo recommended for some systems
• Battery Mounts• Connections always at Aft• Immovable on all 3 axis
− Zip Tie/Velcro/Mechanical Fasteners
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AV Bay
Switches• Mount Internally
• More Aerodynamic• Avoids Shearing
• Wiring• Solder• Terminal Blocks
• Must be Vibration/Bounce Resistant• Mount with “On” in the Down Position
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AV Bay
Static Ports• Required for Barometric Sensors• Recommend 3 or more ports• Port Sizing
• DP=Diameter of Port
• VAB=Volume of AV Bay
• NP=Number of Ports
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Electronics
• Dual Deployment Altimeters• Always have a Barometric Sensor• May have Accelerometers, GPS, or
Timers• Ex. Co-Pilot, Marsa54, XTRA, …
• Timers, etc may be used but are not recommended.
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Electronics
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Electronics
Altimeter Configuration• Altimeter Dependent but …• 1st Deployment (Drogue) at Apogee• 2nd Deployment (Main) at ??? ft AGL
• Parachute Opening Time− Parachute Size− Bridle Length
• Wind Conditions
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Ejection Charges
• Under 25,000 feet• Solutions include Canisters or Surgical
Tubing• Typically on AV Bay Bulkhead
• Over 25,000 feet or CO2
• Requires Airtight Chamber
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Ejection Charges
• Sizing Based on Parameters• Deployment Volume• Shear Pin Size & Number
• No Shear Pins - Coefficient of Friction
• Mass of Ejected Components• Desired Ejection Velocity• Contingency Factor
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Ejection Charges
• Ejection Pressure (PE)
• Nose Cone Force (FNC)
• Requisite Black Powder using Ideal Gas Law (mBP)
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WNC= Weight of Nose ConeNC = Velocity of Nose ConeNSP = Number of Shear PinsSP = Pin Shear StrengthFNC = Nose Cone ForceC = Contingency FactorANC = Area of Nose Cone Base
VRB= Volume of Recovery BayRBP = BP Specific Gas ConstantTBP = BP Combustion Temperature
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Ejection Charges
• Online Calculators Inadequate• Don’t Handle Shear Pins• Don’t Handle Nose Cone Mass• Don’t Handle Desired Exit Velocity
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Attachment Points
• Use Appropriate Hardware
• Don’t Use
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Plastic Loops - Recipe for Disaster
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Attachment Points
• Apogee deployments typically experience 20 to 25g’s
• Validate Strength of Materials• Hardware Working Load Limit (WLL)• WLL/Weight = X g’s (Maximum)• Evaluate Bulk Plates and Joints
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Attachment Points
• Install Correctly• Use Washers to Distribute Load• Fabricate needed Parts• Secure Nuts
• Loctite• Nylon Inserts• Cotter Pins
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Attachment Points
Bridle (Shock Cord)• Knots
• Bowline• Follow Thru Figure 8• Others significantly weaken cord
• Sewn Loops (Stronger than Knots)• Thread Material same as Bridle• Use Rectangle with Cross Pattern
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Attachment Points
Bridle (Shock Cord)• Provide Thermal Protection• Don’t Ignore Material Fatigue &
Thermal Shock• Replace Periodically (every 10 flights
or less)
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Parachutes & Packing
• Drogue Chute• High Velocity Deployment Implies Higher
Strength Requirements
• Main Chute• Shock Forces Controllable based on Drogue
Chute Selection
• Provide Thermal Protection• Heat Shield, Deployment Bag, Cellulose,
Piston, Baffles or use Kevlar Materials
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Parachutes & Packing
• Parachute Sizing• where:
• W = Total Weight
• ve = Desired Descent Velocity
• CD = Parachute Drag Coefficient = Air Density• S = Surface Area of Parachute
• Diameter determined by Shape30
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Parachutes & Packing
Folding Instructions1. Fold with shroud lines as
shown2. Make one last fold over
shroud lines3. Fold top end over end until
you reach the bottom edge4. Connect to bridle5. Insert thermal protection6. Insert into airframe
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Summary
• Success Factors• Physical Design & Construction• Proper Sizing & Testing
• Charges, Parachutes, Bridles, Hardware
• Avionics Configuration• Use of Appropriate Materials
• Thermal Protection, Fatigue Assessment
• Checklist, Checklist, Checklist
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What can happen?
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References
• Modern High Power Rocketry 2; Canepa, Mark; Trafford Publishing, 2005
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Selected Websites
• http://www.offwegorocketry.com/• http://www.tripolimn.org/links
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