University of Iowa USLI

Slides:

Advertisements

Similar presentations

Preliminary Design Review. Rocket & Payload Schematic.

Advertisements

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

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

U NIVERSITY OF F LORIDA T HE M OST I NTERESTING R OCKET IN THE W ORLD.

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.

Project Λscension. Vehicle Dimensions Pad Weight: 28.1 Ib Length: in (9 ft. 4.5 in) Diameter: 6 in Fin Semi-Span: 6 in.

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.

Launch Vehicle  Launch Vehicle Summary  The length of the rocked is inches, and the mass is ounces.  We have a dual Deployment Recovery.

Illinois Space Society Tech Team USLI FRR Presentation.

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.

Project Λscension. Vehicle Dimensions Weight: 87.2N/19.6Ib Length: in. Diameter: 6in. Fin Semi-Span: 6in.

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.

University of Arkansas Senior Project- When Pigs Soar.

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.

University of Florida Rocket Team Critical Design Review Presentation.

Critical Design Review Presentation Jan. 20, 2011.

AAE 450 Spring 2008 Tim Lorenzana 1/16/2008 Avionics Recovery/Termination.

Harvard-Westlake Rocketry Club SLI FRR.

University of Arkansas Senior Project- When Pigs Soar.

Critical Design Review- UCF Jeremy Young Anthony Liauppa Erica Terry, Emily Sachs Kristen Brightwell Gillian Smith 1.

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.

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.

NUSTA RS NASA Student Launch MAV Challenge 2016 Preliminary Design Review 6 November 2015 Northwestern University | 2145 Sheridan Road | Evanston, IL

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 

Critical Design Review Presentation Project Nova.

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

Critical Design Review Presentation Alabama Rocket Engineering Systems (ARES) Team The University of Alabama.

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

Preliminary Design Review Presentation

Preliminary Design review

Critical Design Review Presentation

2018 First Nation Launch - Flight Readiness Review

NASA USLI Preliminary Design Review

Critical Design Review February 2, 2015

November 7, 2014.

Project Lead: Austin Brenner

November 7, 2014.

Critical Design Review

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

2019 First Nation Launch – CDR Virtual Review

Plantation High SL team 1

2019 First Nation Launch – Oral Presentation

Presentation transcript:

University of Iowa USLI FRR

AGSE Design/Dimension Packed Dimensions 3.5’ X 6’ X 3-9’ Rail Size 1” Weight 100lbs

AGSE Key features Robotic Arm 360 Degree Rotation 20” Reach 11 oz Grip Strength Program Language with Computer Communication with Launch Vehicle Stop Switch on computer interface of automated program

AGSE/Launch Vehicle Integration Contact Sensor Ignitor Placement via servo linear actuator

Requirement Verification for AGSE Robotic arm testing and code verification Logic integration with servo winch and servo linear stage Safety Stop switch test on computer code

Launch Vehicle Design/Dimensions Height: 2.38m Diameter: 10.2cm Weight: 6.23kg

Key Launch Vehicle Design Features Dual Deployment system Rotating Payload Bay No Drag System

Motor Description Motor tested: K570 Final Motor: K630 Thrust-Weight Ratio: Test: 13.95 Final: 12.89

Flight Statistics Motor: Cesaroni K630 Thrust-to-Weight Ratio: 12.89 Rail Exit Velocity: 77.1 ft/s (23.5 m/s) Streamers Manufacturer: Sunward Group Ltd. Size: 5 x 50 in (12.7 x 127 cm) Parachute Manufacturer: Angel Chute Size: 52 in diameter (132.1 cm diameter) Terminal Velocity: 21.4 ft/s (6.52 m/s) Mass: 13.7 lbs (6.2 kg) Mass margin: 2 lbs (0.91 kg) Stability: 2.41 cal Kinetic Energy Section 1: 19.8 ft-lbs (26.8 N-m) Section 2: 12.8 ft-lbs (17.4 N-m) Section 3: 51 ft-lbs (69 N-m)

Altitude and Drift Max altitude tested: 6053 ft (1845 m) Max Predicted: 5274.4 ft (1608 m) Drift tested: 3710.6 ft(1131 m) Drift Predicted

Test Plan/Procedure Electronic Testing- recovery, payloadbay interface Drag System Testing- low torque, high risk Payload Bay Testing- rotation test passed

Full Scale Test Flight Data Recovery hand test Recovery ground test Recovery full test

Requirements Verification Strength- Material specs and full test Stability- Simulation and full test Recovery- Ground and full test Payload Secured- Payload test

Questions