NASA SLI 2010 Mulberry Grove High School Flight Readiness Review Measurement of UVB Radiation Absorption by Cloth Material at Different Altitudes and Measurement.

Slides:

Advertisements

Similar presentations

University of Florida PDR Presentation. Vehicle Design Diameter: 5.86 Length: 135 Static Stability Margin: 1.4 Total Weight: 23.6 lbs.

Advertisements

Preliminary Design Review. Rocket & Payload Schematic.

Northwestern University Space Technology and Rocketry Society (NUSTARS) NASA Student Launch Flight Readiness Review March 16, 2015.

P RELIMINARY D ESIGN R EVIEW University of North Dakota Frozen Fury Rockety Team.

Student Launch Project Preliminary Design Review January 10, 2014.

Illinois Space Society Tech Team USLI CDR Presentation.

Project Λscension. Vehicle Dimensions Weight: 19.6 Ib Length: in (9 ft. 4.5 in) Diameter: 6 in Fin Semi-Span: 6 in.

St. Vincent – St. Mary CDR Presentation NASA Student Launch Initiative.

Our Mission Statement  Launch a high-power rocket to an altitude of one mile carrying the Operation: Epic Beep payload package. At lift off, the rocket’s.

NASA SLI 2010 Mulberry Grove High School Critical Design Review Measurement of UVB Radiation Absorption by Cloth Material at Different Altitudes and Measurement.

Flight Readiness Review March Vehicle Criteria Testing and vehicle design Bulkheads: 9-Ply ½” birch plywood made by Public Missiles, Ltd or ¼ inch.

NASA CDR Presentation Spring Grove Area High School.

St. Vincent – St. Mary FRR Presentation NASA Student Launch Initiative.

Windward Community College University of Hawaii

Student Launch Project Critical Design Review February 28, 2014.

Flight Readiness Review. Intimidator 5: 5” diameter, 10’ length, 47 lbs  Motor: Aerotech L1300R 4556 N-Sec of impulse  Predicted altitude 5203’- RockSim.

Critical Design Review. Intimidator 5: 5” diameter, 10’ length, 45 lbs  Motor: Aerotech L1300R 4556 N-Sec of impulse  Predicted altitude RockSim.

Flight Readiness Review Atomic Aggies. Final Launch Vehicle Dimensions Diameter 5.5” Overall length: inches Approximate Loaded Weight: lb.

Critical Design Review of “Mach Shock Reduction” Phase II January 2008 Statesville, NC.

Illinois Space Society Tech Team USLI FRR Presentation.

CDR Clear Lake's Team Rocket 2929 Bay Area Blvd. Houston, TX

Rocket Based Deployable Data Network University of New Hampshire Rocket Cats Collin Huston, Brian Gray, Joe Paulo, Shane Hedlund, Sheldon McKinley, Fred.

Rocket Based Deployable Data Network University of New Hampshire Rocket Cats Collin Huston, Brian Gray, Joe Paulo, Shane Hedlund, Sheldon McKinley, Fred.

Critical Design Review Presentation Jan. 20, 2011.

Preliminary Design Review “Analysis of Atmospheric Cosmic Radiation Distribution as a Function of Altitude” Steven Schroeder-Program Manager Damon Emerson-Rocket.

Student Launch Project Flight Readiness Review April 21, 2014.

 Vehicle dimensions, materials, and justifications  Static stability margin  Plan for vehicle safety verification and testing  Baseline motor selection.

Windward Community College University of Hawaii

Safety ► The safety officer for the entire team is Maia Madrid. ► During launch we will follow NAR safety rules and regulations. ► We will follow standard.

Flight Readiness Review Team Hawaii. Vehicle Properties Diameter (in)6 inches Length (in)127 inches Gross Liftoff Weight (lb)50.25 lb Launch Lug/button.

3/19/09. Animal Motor Works (AMW) K475WW High Power Rocket Motor. 54 mm casing, 40.3 cm long, 2.9 seconds burn time, 1394 N-sec total impulse, and

The Rocket Men Project One Giant Leap. Final Launch Vehicle Dimensions Rocket Length in. Rocket Mass- 171 oz. Top Body Tube Length in. Bottom.

The Comparative Analysis of Airflow Around a Rocket.

FRR Presentation IF AT FIRST YOU DON’T SUCCEED, TRY AGAIN… AND AGAIN AND AGAIN AND AGAIN.

Flight Readiness Review Student Launch Initiative SCS Rocket Team Statesville Christian School April 2, 2008.

The Comparative Analysis of Airflow Around a Rocket.

University of Florida Rocket Team Critical Design Review Presentation.

Critical Design Review Presentation Jan. 20, 2011.

Harvard-Westlake Rocketry Club SLI FRR.

WINDWARD COMMUNITY COLLEGE UNIVERSITY OF HAWAII

HARDING UNIVERSITY A Study of Atmospheric Properties as a Function of Altitude Flying Bison.

Atomic Aggies CDR. Final Launch Vehicle Dimensions Diameter 5.5” Overall length: inches Approximate Loaded Weight: lb.

USLI Flight Readiness Review Harding University Flying Bison 2010 USLI Rocket Team.

Flight Readiness Review “Analysis of Atmospheric gamma radiation as a Function of Altitude by means of Scintillator Probe” St. Thomas High School, Houston,

Project Ares University of Central Florida NASA Student Launch 1/28/2015.

The Rocket Men Project One Giant Leap. Dimensions Rocket Length in. Rocket Mass- 171 oz. Top Body Tube Length in. Bottom Body Tube Length-

Hemodynamics Star Splitters 4-H Club Two Rivers, WI Hemodynamics.

HARDING UNIVERSITY FLYING BISONS A Study of Atmospheric Properties as a Function of Altitude Flight Readiness Review.

University Student Launch Initiative Preliminary Design Review University of Illinois at Urbana-Champaign Team Rocket.

NUSTA RS NASA Student Launch MAV Challenge 2016 Critical Design Review 15 Janurary2015 Northwestern University | 2145 Sheridan Road | Evanston, IL

January 14,  Length: inches  Diameter: 6 inches  Mass: oz. / lbs.  Span: 22 inches  Center of Gravity: inches 

FAMU PDR Presentation. Table of Contents Vehicle dimensions, materials, and justifications Static stability margin Plan for vehicle safety verification.

Flight Readiness Review UNIVERSITY OF SOUTH ALABAMA CONNER DENTON, JOHN FAULK, NGHIA HUYNH, KENT LINO, PHILLIP RUSCHMYER, & ANDREW TINDELL MENTOR : RICHARD.

UCF_USLI Preliminary Design Review David Cousin Freya Ford Md Arif Drew Dieckmann Stephen Hirst Mitra Mossaddad University of Central Florida.

Project Aegis Preliminary Design Review Team Members:

Preliminary Design Review Presentation

Preliminary Design review

Critical Design Review Presentation

2018 First Nation Launch - Flight Readiness Review

Sounding Rocket CDR Team Name

Final Readiness Review

Mars Rover CDR Team Name

2019 First Nation Launch – FRR Virtual Review

2019 First Nation Launch – PDR Virtual Review

2019 First Nation Launch – Oral Presentation

Characteristics,Construction, Recovery

2019 First Nation Launch – CDR Virtual Review

Target Altitude Safety Document

2019 First Nation Launch – Oral Presentation

Presentation transcript:

NASA SLI 2010 Mulberry Grove High School Flight Readiness Review Measurement of UVB Radiation Absorption by Cloth Material at Different Altitudes and Measurement of Vehicle Motor Tube/Case Temperatures During Launch Mulberry Grove SLI Team

NASA SLI 2010 Mulberry Grove High School Outline Motor Choice Rocket flight stability in static margin diagram Thrust to weight motor selection in flight stimulation Rail exit velocity Parachute sizes and decent rates Test plans and procedures Full scale flight test Dual deployment avionics test Ejection charge amount test Payload integration feasibility

NASA SLI 2010 Mulberry Grove High School Motor Choice Engine selected  AeroTech  K700W Diameter- 54 mm Length cm Burn time- 3.5 sec Total impulse Ns

NASA SLI 2010 Mulberry Grove High School Rocket Flight Stability in Static Margin Diagram Center of Gravity68” from the nose cone Center of Pressure86.8” from the nose cone

NASA SLI 2010 Mulberry Grove High School Thrust to Weight Motor Selection in Flight Stimulation Ratio of 6.8 to 1

NASA SLI 2010 Mulberry Grove High School Rail Exit Velocity 68ft/s

NASA SLI 2010 Mulberry Grove High School Parachute Sizes and Decent Rates Drogue Parachute Size: 24” Descent Rate:66 ft/s (simulation) 62 ft/s (test flight) Main Parachute Size:9’ Decent Rate:20ft/s (simulation) 26 ft/sec (test flight)

NASA SLI 2010 Mulberry Grove High School Test Plans and Procedures Temperature Experiment Static Testing Four sensors checked for consistency Battery longevity test Data recorded and download to computer Actual Testing Actual test on first full-scale flight

NASA SLI 2010 Mulberry Grove High School Temperature Test Data

NASA SLI 2010 Mulberry Grove High School UVB Experiment Static Testing Sensors tested and calibrated Sensor, CBL2, TI calculator combination tested Triggering to begin recording tested Data recording tested (limitation of 100 data points) Transfer of data tested No dynamic testing performed.

NASA SLI 2010 Mulberry Grove High School Small Scale Test Flight Flight Test Report

NASA SLI 2010 Mulberry Grove High School Full Scale Flight Test #1 February 28, 2010 Recovery Unsuccessful Anomalies during lift-off Flight Analysis Launch Pad Camera Hand-held Camera

NASA SLI 2010 Mulberry Grove High School Full Scale Flight Test #2 March 18, 2010 Recovery Successful Lift-off, flight, and recovery normal Flight Analysis Launch Pad Camera Hand-held Camera

NASA SLI 2010 Mulberry Grove High School Dual Deployment Avionics Test Altimeter Test Report

NASA SLI 2010 Mulberry Grove High School Ejection Charge Amount Test Black Powder Charge Test Report 2.7 g of black powder will be used. That amount was used in both full-scale flights.

NASA SLI 2010 Mulberry Grove High School Payload Integration Feasibility First full-scale test flight experienced anomalies at take-off. $600 in damage was the result. All UVB sensors were destroyed. Payload bay had structural failure. Payload was re-designed and sensors were placed in pvc pipe to protect them. End caps to couplers reinforced.

NASA SLI 2010 Mulberry Grove High School Payload Integration Feasibility

NASA SLI 2010 Mulberry Grove High School Conclusion Problems encountered during full-scale test flights have been mitigated. Rocket and payload are now ready for a full flight with payload.