2019 First Nation Launch – PDR Virtual Review

Slides:

Advertisements

Similar presentations

PDR Presentation 1. Eric P o Team Leader o Payload Manager o Documentation Manager Michael B o Building Team Manager o Safety Manager Sean K o Outreach.

Advertisements

Preliminary Design Review. Rocket & Payload Schematic.

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

University of North Dakota Frozen Fury Critical Design Review February 2, 2015.

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

Critical Design Review NASA University Student Launch Initiative University of Nebraska–Lincoln

Student Launch Project Preliminary Design Review January 10, 2014.

Illinois Space Society Tech Team USLI CDR Presentation.

U NIVERSITY OF F LORIDA PDR P RESENTATION. O UTLINE Project Organization Vehicle Design Payload Design Recovery System Simulations Future Work.

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.

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

UAA Rocketry Critical Design Review Presentation.

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

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.

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.

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.

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.

Critical Design Review Presentation Jan. 20, 2011.

Harvard-Westlake Rocketry Club SLI FRR.

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.

Preliminary Design Review.  Completed practice launch  New motor selection  Corrected simulations  Improved payload construction  Increased.

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-

D EPARTMENT OF M ECHANICAL AND A EROSPACE E NGINEERING HIGH POWERED ROCKETRY CLUB PDR PRESENTATION 1.

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

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

D EPARTMENT OF M ECHANICAL AND A EROSPACE E NGINEERING HIGH POWERED ROCKETRY CLUB CDR PRESENTATION 1.

PLANTATION HIGH PDR PRESENTATION Team 1. VEHICLE DIMENSION & MATERIALS.

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

Preliminary Design Review Clear Lake High School Team Rocket.

Planetary Lander PDR Team Name

Project Aegis Preliminary Design Review Team Members:

Preliminary Design Review Presentation

College of Engineering

Critical Design Review Presentation

2018 First Nation Launch - Flight Readiness Review

NASA USLI Preliminary Design Review

Preliminary Design Review

Critical Design Review February 2, 2015

Sounding Rocket PDR Team Name

Project Lead: Austin Brenner

Critical Design 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 – Oral Presentation

2019 First Nation Launch – CDR Virtual Review

Plantation High SL team 1

Target Altitude Safety Document

University of Iowa USLI

2019 First Nation Launch – Oral Presentation

Presentation transcript:

2019 First Nation Launch – PDR Virtual Review [insert team name here]

Team Information [school and team name] [mentor name] [advisor name] [team member introductions]

Launch Vehicle [discuss general design, dimensions - justification] [discuss motor selection - justification]

Launch Vehicle Performance [discuss flight stability, static margins] [discuss thrust-to-weight ratio, rail exit velocity]

Avionics Subsystem [discuss the avionics bay design – location in vehicle] [discuss number of altimeters, power, wiring]

Recovery Subsystem [discuss parachute recovery scheme – sizes, descent rates] [discuss parachute locations and ejection events]

Mission Performance [discuss mission performance predictions (simulations)]

Payload / Experiment [discuss payload design – including general dimensions] [discuss key features of the payload]

Questions?