Presentation is loading. Please wait.

Presentation is loading. Please wait.

2018 First Nation Launch - Flight Readiness Review

Published byAlexander McDowell Modified over 6 years ago

Similar presentations

Presentation on theme: "2018 First Nation Launch - Flight Readiness Review"— Presentation transcript:

1 2018 First Nation Launch - Flight Readiness Review
[insert team name here]

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

3 Launch Vehicle [discuss general design and dimensions]
[discuss key features] [discuss motor selection] [discuss mass statement]

4 Launch Vehicle Performance
[discuss rocket simulation method – rocksim, openrocket or other] [discuss flight stability, static margins] [discuss thrust-to-weight ratio, rail exit velocity]

5 Avionics [discuss the electronics bay design – location in vehicle]
[discuss number of altimeters, type, manufacture] [discuss vent holes size and location] [discuss programming interface for altimeters]

6 Recovery [discuss parachute recovery scheme – sizes, descent rates, location in vehicle] [discuss ejection charges required] [discuss kinetic energy at landing] [discuss tracking devices]

7 Payload / Experiment [discuss payload design – including general dimensions] [discuss key features of the payload] [discuss any testing completed] [discuss payload electronics] [discuss how the payload is integrated into/with the vehicle]

8 Questions?

Download ppt "2018 First Nation Launch - Flight Readiness Review"

Similar presentations

Preliminary Design Review. Rocket & Payload Schematic.

Preliminary Design Review. Rocket & Payload Schematic.
Northwestern University Space Technology and Rocketry Society (NUSTARS) NASA Student Launch Flight Readiness Review March 16, 2015.

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.

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 2012-2013.

Critical Design Review NASA University Student Launch Initiative University of Nebraska–Lincoln
Student Launch Project Preliminary Design Review January 10, 2014.

Student Launch Project Preliminary Design Review January 10, 2014.
Illinois Space Society Tech Team USLI CDR Presentation.

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.

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: 112.5 in (9 ft. 4.5 in) Diameter: 6 in Fin Semi-Span: 6 in.

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

St. Vincent – St. Mary FRR Presentation NASA Student Launch Initiative.
UAA Rocketry Critical Design Review Presentation.

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.

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.

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.

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 5715- 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: 117.14 inches Approximate Loaded Weight: 35.25 lb.

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.

Critical Design Review of “Mach Shock Reduction” Phase II January 2008 Statesville, NC.
Illinois Space Society Tech Team USLI FRR Presentation.

Illinois Space Society Tech Team USLI FRR Presentation.
CDR Clear Lake's Team Rocket 2929 Bay Area Blvd. Houston, TX 77059.

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.

Similar presentations

Ads by Google