1 / 27

CDR 2011

CDR 2011. Windward Community College. Todd & Model Rocket. Project. Rocket: Leo Hano Payload: Hula-hoop. Characteristics . GPSFlight in nose cone Variable Drag Configuration (VDR) Four fin design Avionics Featherweight Raven-2 PerfectFlight MAWD Dual Deployment. Motor: L1300R

inga
Download Presentation

CDR 2011

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript

  1. CDR 2011 Windward Community College

  2. Todd & Model Rocket

  3. Project Rocket: Leo Hano Payload: Hula-hoop

  4. Characteristics • GPSFlight in nose cone • Variable Drag Configuration (VDR) • Four fin design • Avionics • Featherweight Raven-2 • PerfectFlight MAWD • Dual Deployment

  5. Motor: L1300R • Thrust/Weight: 6.49 • Total Impulse: 4567.0 N • Casing: RMS 98/5120 • Average Thrust: 1300.0 N • Peak Thrust: 1,552.5 N • Burn Time: 3.5 Motor Selection

  6. Flight Profile • Boost Phase • Coast Phase • Apogee • Drogue Deployed • Rapid Decent Phase • 82 ft/sec • Main Decent Phase • 22 ft/sec

  7. Parachutes Main Chute • 144in (12 feet) • Decent Rate:22 feet per second Drogue Chute • 42in (3 and 1 half feet) • Decent Rate: 82 feet per second

  8. Overview

  9. Recovery Avionics Block Diagram

  10. Testing • Model Rocket Launches: On going • Third Saturday of every month • Duel Deployment Avionics Test: February 26, 2011 • Full Scale Low Power Launch (FSLP): March 13, 2011 • FSLP Rain Date: March 20, 2011 • K560 • Altitude:1,930 feet • Max Speed: 299 feet/sec • Max Acceleration: 407 feet/sec/sec • Estimated Flight Duration: 3 minutes

  11. Payload Parts List - Hula-hoop 1 • BS2pe Micro Controller • 12-bit ADC • Temperature sensor

  12. Hula-hoop 1 Block Diagram A/D BS2pe Temp Sensor

  13. Payload Parts List – Hula-hoop 2 • BS2p Micro Controller • EEPROM • 24-bit ADC • Temperature sensor • coil • 12-bit ADC • Temperature sensor • 3-axis accelerometer (for comparison) • Consists of one coil

  14. Hula-hoop 2 Design SPI Data Bus Accelerometer BS2p Coil # 1 A/D #1 2 I C Bus Temp Sensor # 1 EEPROM A/D #2 Temp Sensor # 2

  15. Payload Parts List – Hula-hoop 3 • BS2p Micro Controller • Eight EEPROM • Three 24-bit ADC • Temperature sensor • coil • 12-bit ADC • Temperature sensor • 3-axis accelerometer (for comparison) • Consists of three perpendicular coils around a non-magnetic sphere

  16. Preliminary Design For Hula-hoop 3 SPI Data Bus Accelerometer BS2p Coil # 1 A/D #1 Temp Sensor # 1 Coil #2 A/D #2 2 I C Bus Temp Sensor # 2 Coil #3 A/D #3 Temp Sensor # 3 EEPROM A/D #4 Temp Sensor # 4

  17. Model Launch/Avionic Complete Rocket Complete Booster Complete FSLP Rain Date Avionics Test Model Launch USLI FSLP 5 Feb 13 19 20 5 19 12 - 18 26 March April Time Line

  18. Rocket Construction Time Line • Begin Construction: February 1 • Booster Complete: February 5 • Avionics Complete: February 19 • Dual Deployment Avionics Test: February 26 • Rocket Construction Complete: March 5

  19. Outreach

  20. Education Outreach Endeavors • Community Outreach • Boys/girls Club etc. • Model Rocket Launches • School Involvement • Payload Projects • ARCHES • TARC • Military Involvement • Reach Across the Pacific • KMCAS • O’Lelo

  21. Mahalo Please don’t hate us because we live in Hawaii

More Related