Staging in High Powered Rocketry Presenters: Mai Vo, Carson Dobbs - - PowerPoint PPT Presentation

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Staging in High Powered Rocketry Presenters: Mai Vo, Carson Dobbs - - PowerPoint PPT Presentation

Staging in High Powered Rocketry Presenters: Mai Vo, Carson Dobbs Authors: Carson Coursey, Mai Vo, Carson Dobbs October 25th, 2018 What is staging? 1/16 Why use multiple stages? Makes rocket more efficient Gets rid of inert mass o


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Staging in High Powered Rocketry

Presenters: Mai Vo, Carson Dobbs Authors: Carson Coursey, Mai Vo, Carson Dobbs

October 25th, 2018

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What is staging?

1/16

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Why use multiple stages?

  • Makes rocket more efficient
  • Gets rid of inert mass
  • Saves fuel
  • Makes rocket able to go higher
  • Without the extra mass, rocket is able to go further
  • Use the fueled saved to go higher
  • It’s cool

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Types of Staging

Inline Staging (Single Sustainer)

  • Vertically stacked boosters and sustainer
  • Each booster is discarded after motor burnout

Parallel Staging (Single Sustainer)

  • Similar to Air Starting
  • Boosters are externally attached to the sustainer
  • Each booster separates from the sustainer after its motor burns out

Parasite Staging (Multiple Sustainers)

  • Similar to Air Starting
  • Sustainers are externally attached to the booster
  • Each sustainer separates after booster burn out

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Inline Staging

  • Used in most projects of this type, as well as

projects at the highest level: Saturn V, F9, etc.

  • Staging type we’ll most likely go with
  • It’s the most common for HPR
  • It’s the most applicable for our objective
  • Nobody has said anything about a different type
  • f staging

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Difficulties of Staging

  • 2 of Everything
  • (ignitions, separations, recovery devices,... rockets)
  • Separation
  • Structure required
  • Separation implement
  • Timing
  • Ignition
  • Air start
  • Delay
  • Altitude calculations

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SLIDE 7

Phases of Staged Flight

  • 1. Booster Ignition - Typical
  • 2. Booster Ascent - Typical, more complex
  • 3. Coast + Separation - New
  • 4. Sustainer Ignition - New
  • 5. Sustainer Flight - Typical
  • 6. Recovery - Typical, more complex

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Image and info from UAH SHC rocketry report

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SLIDE 8

Separation - Required Components

  • Interstage Structure
  • Coupler
  • Black powder charge/CO2 Can
  • Shear pins
  • Possible avionics bay in the interstage
  • Some sort of nozzle cap or “Piston” that comes off during

sustainer ignition

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Separation Solutions

  • UAH - 3D Printed Interstage w/ shear pins
  • Blue is interstage structure ejected via

black powder

  • White “piston” comes off during sustainer

ignition

  • Red is boat tail fairing, attached to centering

rings

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Separation Solutions 2

  • Princeton - Aluminum Interstage
  • Highly load bearing
  • Slip fit to sustainer motor
  • Seemingly ejection by sustainer

ignition

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Ignition - Air Start

  • Possible Failures:
  • Stage ignition failure
  • Late stage ignition
  • Coupler malfunction
  • Early, late or no deployment
  • Difficulties
  • Not on launch rail
  • Electronic Accuracy
  • Ignition delay (later slides)

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Ignition - Air Start

  • Required Hardware
  • Standard avionics hardware (battery, accelerometer, computer,

timer)

  • Ignition hardware (e-match, motor igniter)
  • Solutions
  • Most projects seemed to not have much info on how to air start
  • Simple timed ignition from the avionics
  • Most likely varies based on design choices, altitudes, etc.

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Ignition - Altitude Calculation

  • Closely tied to Ignition Delay
  • Time the sustainer ignition so that high velocity is maintained

for a vertical flight.

  • Ignition at too low of a velocity will cause the sustainer to

drift and ignite the motor in a non-vertical direction. Velocity starts decreasing upon stage separation, so the sooner ignition begins, the straighter the sustainer will fly.

  • However, if coast is prolonged, the sustainer is able to reach

higher altitudes.

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Ignition - Delay

  • How long the sustainer coasts before

ignition will have a measurable effect on

  • ur apogee
  • There is a sweet spot that can be

determined by running simulations (RASAero, etc) to achieve 30,000 ft

  • All that would need to be changed to

put in the correct time would be the code/timer

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Useful Links

  • http://space.uah.edu/assets/files/manuscript_Hunter_04267

.pdf

  • http://rocket.gtorg.gatech.edu/files/slides/Staging_Clusterin

g_and_Complexity.pdf

  • http://s605282183.onlinehome.us/wp-content/uploads/201

6/01/Staging-Air-Starting.pdf

  • https://www.rocketryforum.com/threads/need-help-with-hi

gh-powered-staging.57697/

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Useful Links

  • https://www.rocketryforum.com/threads/so-maybe-ill-try-a-

three-stager.66850/

  • http://www.spaceportrocketry.org/Motor%20Staging.html

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The End.