Flight Readiness Review
|
|
|
- Hortense Cobb
- 5 years ago
- Views:
Transcription
1 Flight Readiness Review University of Illinois at Urbana-Champaign NASA Student Launch Illinois Space Society 1
2 Overview Illinois Space Society 2
3 Launch Vehicle Summary Javier Brown Illinois Space Society 3
4 Flight Profile Illinois Space Society 4
5 Current Launch Vehicle Design Nose cone 1) Ejection charge at apogee 3) Nose cone separation and parachute deployment at 1000 feet Upper body tube Coupler 2) Drogue deployment at apogee Booster tube Illinois Space Society 5
6 Vehicle - Major Dimensions Total Length: 130 Total Mass: 43.5 lb. Nosecone: 30 Upper Airframe: 48 Payload Bay: 14 Avionics Coupler: 16 Booster Frame: 48 Outer Diameter: 6 Root Chord (Fins): 12 Illinois Space Society 6
7 Vehicle - Mass Statement Mass of rocket increased due to heavier nosecone and ballast Heaver nosecone required ~1 lb of ballast in top centering ring for stability Mass Breakdown Subsystem Mass (lbm) Structures Recovery 8.32 Motor 9.32 Rover 2.02 Platform 3.42 Total 40.7 Illinois Space Society 7
8 liftoff: 2.48 calibers Current CP location: Static CG location: Vehicle - Stability Ballast utilized just above top most centering ring to guarantee and ideally stabilized vehicle. Illinois Space Society 8
9 Vehicle - Propulsion Motor: L1420R-P Diameter: 2.95 (75 mm) Max thrust: 374 lbf Total impulse: 1038 lbf s Burn time: 3.18 s T/W ratio: 8.49 Off-rail speed: 61.4 ft/s 3 8 Aircraft grade plywood centering rings RMS 75/5120 Casing Illinois Space Society 9
10 U-Bolt connections for strength 1/4-20 T-nuts/Bolts for permanent attachments Two rotary switches Parachutes Main: Iris Ultra 96 Drogue: Fruity Chutes Elliptical 18 1/2 Tubular Kevlar shock cord Redundant altimeters 1 TeleMetrum altimeter for altitude and location tracking 1 StratoLogger altimeter for altitude tracking Airframe - Recovery Illinois Space Society 10
11 U-Bolt connections for strength Two rotary switches Parachute Nosecone: SkyAngle 40 1/2 Tubular Kevlar shock cord Redundant altimeters 1 Telemetrum altimeter for altitude and location tracking 1 StratoLogger altimeter for altitude tracking Nosecone - Recovery Illinois Space Society 11
12 Ejection Charges Number of shear pins based on section weights, accelerations, and shear pin maximum forces Black powder charges calculated with pressures and forces applied to the bulkhead Joint Joint and Shear Pin Properties Max Accelerati on Mass Above Joint [lbm] Max Shear Force [lbf] # of Shear Pins Required g g g Joint # of Shear Pins Amount of Black Powder Needed Diameter [in] Length [in] Illinois Space Society 12 Area [in^2] Force [lbf] Pressure [psi] Grams of FFFFG Black Powder
13 Full vehicle verification plan found in FRR Vehicle Verification Plan Major verification tasks Verified aerodynamics and construction procedure with subscale creation and flight Increased simulation accuracy Small-scale and large-scale testing of components Verified vehicle design and manufacturing during fullscale test flight Illinois Space Society 13
14 Predictions determined using OpenRocket. Terminal Velocities Nosecone ft/s Upper Airframe and Booster Frame 1 st separation: Drogue 103/85 ft/s Main ft/s Kinetic Energy Kinetic Energies Booster Frame ft lbf Avionics Coupler ft lbf Upper Airframe w/ Payload ft lbf Nosecone ft lbf All kinetic energies are within specified threshold of 75 ft lbf Illinois Space Society 14
15 Drift Predictions Predictions determined using OpenRocket. All predictions are well within the stipulated threshold of 2640 ft. Section Drift in 0 mph winds (ft) Drift in 5 mph winds (ft) Drift in 10 mph winds (ft) Drift in 15 mph winds (ft) Drift in 20 mph winds (ft) Booster and Upper Airframe Nosecone Illinois Space Society 15
16 Computational Fluid Dynamics CFD performed to verify integrity of pressure readings for nosecone altimeters Full 3D simulation done with ANSYS Results show that pressure at nosecone shoulder is very close to pressure along body Illinois Space Society 16
17 Launched on February 17 th, 2018 in Princeton, IL Launch, ascent, and descent was successful Ineffective deployment of nosecone parachute Damage to nosecone shoulder and threaded rod Altimeters successfully reported data Full Scale Test Flight Illinois Space Society 17
18 Figure of StratoLogger vs OpenRocket Nosecone and coupler avionics data match well Further proof of integrity of nosecone pressure reading Actual flight data over-performed compared to OpenRocket predictions Motor overperformance Overestimated mass Illinois Space Society 18
19 Full Scale Test Flight Ground Track TeleMetrum GPS location superposed onto Google Earth ground image Drift distance of 2137 ft., which is below competition requirement of 2500 ft. Illinois Space Society 19
20 Hard impact to shoulder and bulkhead of nosecone Fiberglass shoulder severely cracked Protruding end of threaded rod bent Bulkhead alignment to nosecone compromised Damages to Nosecone Illinois Space Society 20
21 Minor delamination on surface of blue tube Caused by snow packed into section from parachute dragging section on ground Most fraying near rotary switch cutout Slight swelling and warping near tips Makes fit with nosecone slightly difficult Damages to Body Tube Illinois Space Society 21
22 Deployable Rover Payload Ryan Noe and Destiny Fawley Illinois Space Society 22
23 NASA Student Launch Requirements: Payload Requirements Teams will design a custom rover that will deploy from the internal structure of the launch vehicle. At landing, the team will remotely activate a trigger to deploy the rover from the rocket. After deployment, the rover will autonomously move at least 5ft. (in any direction) from the launch vehicle. The rover will deploy a set of solar panels once it has traveled the 5ft. Required by the competition. Internal Team Requirements: Upon landing, the orientation mechanism must be able to rotate the rover to a position in which it can properly deploy. After the rover has deployed the solar panels, the Arduino will receive readings from the solar panels. 5 lb. limit 5.95 diameter x 14.5 length Illinois Space Society 23
24 Payload Overview Rover Orientation Mechanism Illinois Space Society 24
25 Rover Design Iterations Version 1 (Proposal) Version 2 (PDR) Final Design Version 3 (CDR) Illinois Space Society 25
26 Wheel Design Iteration Windmill wheels Five point wheels Less jarring Optimized grip Improved servo mount Illinois Space Society 26
27 Rover Overview Miniaturized Off-Road Remote Terrain Explorer (MORRTE) Consists of 3 segments attached with steel axles All 3D-printed components Each segment is specific to certain electronics Front Segment Middle Segment Back Segment Illinois Space Society 27
28 2 solar cells Two, five point wheels Two servo motors Servo-driven hinge Orientation system latching loop Electronics: SD Card Reader Power Boost 3.7V Li-ion Battery Front Segment of the Rover Illinois Space Society 28
29 Camera and camera cover mounted on bridge 2 servo motors 2, 5 point wheels Electronics: Arduino Micro MPU 6050 HC-12 Middle Segment of the Rover Illinois Space Society 29
30 6V NiCd battery Servo connection panel Safety bridge 2 servo motors 2, 5 point wheels Orientation system latching loop Back Segment of the Rover Illinois Space Society 30
31 Rover Prototyping First Round of Prototyping Final Round of Prototyping Prototyping Changes Rover segment modifications Wheel modifications Bridge designs Solar cells hinge/bridge assembly Camera mount Illinois Space Society 31
32 Orientation System Overview System to ensure rover leaves airframe upright Bulkhead screwed to Upper Airframe Platform rotated by servo motor Controlled by Arduino Micro system Illinois Space Society 32
33 Orientation System Design Iterations Version 1 (Proposal) Version 2 (PDR) Final Design Version 3 (CDR) Illinois Space Society 33
34 AL6061 Bulkhead AL6061 Platform 3D-printed electronics Cover Aluminum Axle & Gear Electronics Arduino Micro Continuous Rotation Servo 2x Servo MPU6050 9DOF Accelerometer/Gyroscope HC-12 Transceiver Module PowerBoost 500C 6V Ni-Ca Battery Pack 3.7V Li-ion Battery Orientation System Hardware Illinois Space Society 34
35 Orientation System Prototyping Early prototype: change motor speed using orientation Successfully used MPU6050 accelerometer data for orientation Early prototyping changed motor speed based on breadboard orientation critical to the orientation system Illinois Space Society 35
36 Electrical Schematics Orientation System Schematic Rover Schematic Illinois Space Society 36
37 Payload System Software Two systems activated shortly before rocket assembly Rover and Orientation System act semi-independently Illinois Space Society 37
38 Rover Testing Successfully tested Ambulated from body tube Maneuvered multiple terrains Over a hill On grass and dirt Regular, tile floor Illinois Space Society 38
39 Orientation System Testing Successfully tested Orientation scheme is successful Latches lock and unlock at the same time Illinois Space Society 39
40 Full Scale Test Flight Payload system flown on full scale test flight Rover attached to orientation system bulkhead with Kevlar cord Orientation system loaded with functional code, no rover code Results: Rover survived intact Solar panels lost upon main chute ejection Front servo horn pulled from threads, back servo PLA arm sheared Rover successfully kept from falling with Kevlar cord Power issue prevented orientation system from properly functioning Orientation system components intact, functional Illinois Space Society 40
41 Payload Future Work Resolve orientation system power issue to ensure battery-only functionality Communications code and capabilities testing Construct, program, and test ground station button Integrate on-off switch on rover and orientation system Demonstrate full payload functionality on second full-scale launch Illinois Space Society 41
42 Safety Courtney Leverenz Illinois Space Society 42
43 Operations Procedure Completed Operations Procedure Illinois Space Society 43
44 Operations Procedure Explanation Verification (SO/A Team Lead) Verification of Critical Operation (SO/A Team Lead) Caution of Hazard Procedure for Correct Operation Illinois Space Society 44
45 Updates Environmental Concerns Spilt and updated Affects to/from project Verification References Cross-sectioned Illinois Space Society 45
46 Questions? Illinois Space Society 46
Critical Design Review
Critical Design Review University of Illinois at Urbana-Champaign NASA Student Launch 2017-2018 Illinois Space Society 1 Overview Illinois Space Society 2 Launch Vehicle Summary Javier Brown Illinois Space
Illinois Space Society Flight Readiness Review. University of Illinois Urbana-Champaign NASA Student Launch March 30, 2016
Illinois Space Society Flight Readiness Review University of Illinois Urbana-Champaign NASA Student Launch 2015-2016 March 30, 2016 Team Managers Project Manager: Ian Charter Structures and Recovery Manager:
CRITICAL DESIGN REVIEW. University of South Florida Society of Aeronautics and Rocketry
CRITICAL DESIGN REVIEW University of South Florida Society of Aeronautics and Rocketry 2017-2018 AGENDA 1. Launch Vehicle 2. Recovery 3. Testing 4. Subscale Vehicle 5. Payload 6. Educational Outreach 7.
NASA SL - NU FRONTIERS. PDR presentation to the NASA Student Launch Review Panel
NASA SL - NU FRONTIERS PDR presentation to the NASA Student Launch Review Panel 1 Agenda Launch Vehicle Overview Nose Cone Section Payload Section Lower Avionic Bay Section Booster Section Motor Selection
Presentation Outline. # Title
FRR Presentation 1 Presentation Outline # Title 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 Team Introduction Mission Summary Vehicle Overview Vehicle Dimensions Upper Body Section Elliptical
Presentation Outline. # Title # Title
CDR Presentation 1 Presentation Outline # Title # Title 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 Team Introduction Vehicle Overview Vehicle Dimensions Upper Body Section Payload
FLIGHT READINESS REVIEW TEAM OPTICS
FLIGHT READINESS REVIEW TEAM OPTICS LAUNCH VEHICLE AND PAYLOAD DESIGN AND DIMENSIONS Vehicle Diameter 4 Upper Airframe Length 40 Lower Airframe Length 46 Coupler Band Length 1.5 Coupler Length 12 Nose
NASA - USLI Presentation 1/23/2013. University of Minnesota: USLI CDR 1
NASA - USLI Presentation 1/23/2013 2013 USLI CDR 1 Final design Key features Final motor choice Flight profile Stability Mass Drift Parachute Kinetic Energy Staged recovery Payload Integration Interface
CRITICAL DESIGN PRESENTATION
CRITICAL DESIGN PRESENTATION UNIVERSITY OF SOUTH ALABAMA LAUNCH SOCIETY BILL BROWN, BEECHER FAUST, ROCKWELL GARRIDO, CARSON SCHAFF, MICHAEL WIESNETH, MATTHEW WOJCIECHOWSKI ADVISOR: CARLOS MONTALVO MENTOR:
Flight Readiness Review Addendum: Full-Scale Re-Flight. Roll Induction and Counter Roll NASA University Student Launch.
Flight Readiness Review Addendum: Full-Scale Re-Flight Roll Induction and Counter Roll 2016-2017 NASA University Student Launch 27 March 2017 Propulsion Research Center, 301 Sparkman Dr. NW, Huntsville
Georgia Tech NASA Critical Design Review Teleconference Presented By: Georgia Tech Team ARES
Georgia Tech NASA Critical Design Review Teleconference Presented By: Georgia Tech Team ARES 1 Agenda 1. Team Overview (1 Min) 2. 3. 4. 5. 6. 7. Changes Since Proposal (1 Min) Educational Outreach (1 Min)
Jordan High School Rocketry Team. A Roll Stabilized Video Platform and Inflatable Location Device
Jordan High School Rocketry Team A Roll Stabilized Video Platform and Inflatable Location Device Mission Success Criteria No damage done to any person or property. The recovery system deploys as expected.
Auburn University. Project Wall-Eagle FRR
Auburn University Project Wall-Eagle FRR Rocket Design Rocket Model Mass Estimates Booster Section Mass(lb.) Estimated Upper Section Mass(lb.) Actual Component Mass(lb.) Estimated Mass(lb.) Actual Component
Auburn University Student Launch. PDR Presentation November 16, 2015
Auburn University Student Launch PDR Presentation November 16, 2015 Project Aquila Vehicle Dimensions Total Length of 69.125 inches Inner Diameter of 5 inches Outer Diameter of 5.25 inches Estimated mass
University of Illinois at Urbana-Champaign Illinois Space Society Student Launch Preliminary Design Review November 3, 2017
University of Illinois at Urbana-Champaign Illinois Space Society Student Launch 2017-2018 Preliminary Design Review November 3, 2017 Illinois Space Society 104 S. Wright Street Room 18C Urbana, Illinois
NASA SL Critical Design Review
NASA SL Critical Design Review University of Alabama in Huntsville 1 LAUNCH VEHICLE 2 Vehicle Summary Launch Vehicle Dimensions Fairing Diameter: 6 in. Body Tube Diameter: 4 in. Mass at lift off: 43.8
Flight Readiness Review March 16, Agenda. California State Polytechnic University, Pomona W. Temple Ave, Pomona, CA 91768
Flight Readiness Review March 16, 2018 Agenda California State Polytechnic University, Pomona 3801 W. Temple Ave, Pomona, CA 91768 Agenda 1.0 Changes made Since CDR 2.0 Launch Vehicle Criteria 3.0 Mission
Project NOVA
Project NOVA 2017-2018 Our Mission Design a Rocket Capable of: Apogee of 5280 ft Deploying an autonomous Rover Vehicle REILLY B. Vehicle Dimensions Total Length of 108 inches Inner Diameter of 6 inches
Preliminary Design Review. California State University, Long Beach USLI November 13th, 2017
Preliminary Design Review California State University, Long Beach USLI November 13th, 2017 System Overview Launch Vehicle Dimensions Total Length 108in Airframe OD 6.17in. ID 6.00in. Couplers OD 5.998in.
NASA USLI PRELIMINARY DESIGN REVIEW. University of California, Davis SpaceED Rockets Team
NASA USLI 2012-13 PRELIMINARY DESIGN REVIEW University of California, Davis SpaceED Rockets Team OUTLINE School Information Launch Vehicle Summary Motor Selection Mission Performance and Predictions Structures
Statement of Work Requirements Verification Table - Addendum
Statement of Work Requirements Verification Table - Addendum Vehicle Requirements Requirement Success Criteria Verification 1.1 No specific design requirement exists for the altitude. The altitude is a
Wichita State Launch Project K.I.S.S.
Wichita State Launch Project K.I.S.S. Benjamin Russell Jublain Wohler Mohamed Moustafa Tarun Bandemagala Outline 1. 2. 3. 4. 5. 6. 7. Introduction Vehicle Overview Mission Predictions Payload Design Requirement
NASA s Student Launch Initiative :
NASA s Student Launch Initiative : Critical Design Review Payload: Fragile Material Protection 1 Agenda 1. Design Overview 2. Payload 3. Recovery 4. 5. I. Sub-Scale Predictions II. Sub-Scale Test III.
UC Berkeley Space Technologies and Rocketry Preliminary Design Review Presentation. Access Control: CalSTAR Public Access
UC Berkeley Space Technologies and Rocketry Preliminary Design Review Presentation Access Control: CalSTAR Public Access Agenda Airframe Propulsion Payload Recovery Safety Outreach Project Plan Airframe
NASA SL Flight Readiness Review
NASA SL Flight Readiness Review University of Alabama in Huntsville 1 LAUNCH VEHICLE 2 Vehicle Overview Vehicle Dimensions Diameter: 6 fairing/4 aft Length: 106 inches Wet Mass: 41.1 lbs. Center of Pressure:
Preliminary Design Review. Cyclone Student Launch Initiative
Preliminary Design Review Cyclone Student Launch Initiative Overview Team Overview Mission Statement Vehicle Overview Avionics Overview Safety Overview Payload Overview Requirements Compliance Plan Team
GIT LIT NASA STUDENT LAUNCH PRELIMINARY DESIGN REVIEW NOVEMBER 13TH, 2017
GIT LIT 07-08 NASA STUDENT LAUNCH PRELIMINARY DESIGN REVIEW NOVEMBER TH, 07 AGENDA. Team Overview (5 Min). Educational Outreach ( Min). Safety ( Min) 4. Project Budget ( Min) 5. Launch Vehicle (0 min)
Overview. Mission Overview Payload and Subsystems Rocket and Subsystems Management
MIT ROCKET TEAM Overview Mission Overview Payload and Subsystems Rocket and Subsystems Management Purpose and Mission Statement Our Mission: Use a rocket to rapidly deploy a UAV capable of completing search
Tacho Lycos 2017 NASA Student Launch Critical Design Review
Tacho Lycos 2017 NASA Student Launch Critical Design Review High-Powered Rocketry Team 911 Oval Drive Raleigh NC, 27695 January 13, 2017 Table of Contents Table of Figures:... 8 Table of Appendices:...
Team Air Mail Preliminary Design Review
Team Air Mail Preliminary Design Review 2014-2015 Space Grant Midwest High-Power Rocket Competition UAH Space Hardware Club Huntsville, AL Top: Will Hill, Davis Hunter, Beth Dutour, Bradley Henderson,
Tacho Lycos 2017 NASA Student Launch Flight Readiness Review
Tacho Lycos 2017 NASA Student Launch Flight Readiness Review High-Powered Rocketry Team 911 Oval Drive Raleigh NC, 27695 March 6, 2017 Table of Contents Table of Figures... 9 Table of Appendices... 11
Critical Design Review Report
Critical Design Review Report I) Summary of PDR report Team Name: The Rocket Men Mailing Address: Spring Grove Area High School 1490 Roth s Church Road Spring Grove, PA 17362 Mentor: Tom Aument NAR Number
Notre Dame Rocketry Team. Flight Readiness Review March 8, :00 PM CST
Notre Dame Rocketry Team Flight Readiness Review March 8, 2018 2:00 PM CST Contents Overview Vehicle Design Recovery Subsystem Experimental Payloads Deployable Rover Payload Air Braking System Safety and
Illinois Space Society University of Illinois Urbana Champaign Student Launch Maxi-MAV Preliminary Design Review November 5, 2014
Illinois Space Society University of Illinois Urbana Champaign Student Launch 2014-2015 Maxi-MAV Preliminary Design Review November 5, 2014 Illinois Space Society 104 S. Wright Street Room 321D Urbana,
University Student Launch Initiative
University Student Launch Initiative HARDING UNIVERSITY Flight Readiness Review March 31, 2008 Launch Vehicle Summary Size: 97.7 (2.5 meters long), 3.1 diameter Motor: Contrail Rockets 54mm J-234 Recovery
AUBURN UNIVERSITY STUDENT LAUNCH PROJECT NOVA II. 211 Davis Hall AUBURN, AL CDR
AUBURN UNIVERSITY STUDENT LAUNCH PROJECT NOVA II 211 Davis Hall AUBURN, AL 36849 CDR January 10, 2019 Contents List of Tables...7 List of Figures...9 1 CDR Report Summary...12 1.1 Payload Deployable Rover...12
The University of Toledo
The University of Toledo Project Kronos Preliminary Design Review 11/03/2017 University of Toledo UT Rocketry Club 2801 W Bancroft St. MS 105 Toledo, OH 43606 Contents 1 Summary of Proposal... 6 1.1 Team
University of Notre Dame
University of Notre Dame 2016-2017 Notre Dame Rocketry Team Critical Design Review NASA Student Launch Competition Roll Control and Fragile Object Protection Payloads Submitted January 13, 2017 365 Fitzpatrick
PRELIMINARY DESIGN REVIEW
PRELIMINARY DESIGN REVIEW 1 1 Team Structure - Team Leader: Michael Blackwood NAR #101098L2 Certified - Safety Officer: Jay Nagy - Team Mentor: Art Upton NAR #26255L3 Certified - NAR Section: Jackson Model
Presentation 3 Vehicle Systems - Phoenix
Presentation 3 Vehicle Systems - Phoenix 1 Outline Structures Nosecone Body tubes Bulkheads Fins Tailcone Recovery System Layout Testing Propulsion Ox Tank Plumbing Injector Chamber Nozzle Testing Hydrostatic
Critical Design Review
Critical Design Review 1/27/2017 NASA Student Launch Competition 2016-2017 California State Polytechnic University, Pomona 3801 W Temple Ave, Pomona, CA 91768 1/27/2017 California State Polytechnic University,
NUMAV. AIAA at Northeastern University
NUMAV AIAA at Northeastern University Team Officials Andrew Buggee, President, Northeastern AIAA chapter Dr. Andrew Goldstone, Faculty Advisor John Hume, Safety Officer Rob DeHate, Team Mentor Team Roster
Student Launch. Enclosed: Preliminary Design Review. Submitted by: Rocket Team Project Lead: David Eilken
University of Evansville Student Launch Enclosed: Preliminary Design Review Submitted by: 2016 2017 Rocket Team Project Lead: David Eilken Submission Date: November 04, 2016 Payload: Fragile Material Protection
Tripoli Rocketry Association Level 3 Certification Attempt
Tripoli Rocketry Association Level 3 Certification Attempt Kevin O Classen 1101 Dutton Brook Road Goshen, VT 05733 (802) 247-4205 kevin@back2bed.com Doctor Fill Doctor Fill General Specifications Airframe:
Critical Design Review
AIAA Orange County Section Student Launch Initiative 2011-2012 Critical Design Review Rocket Deployment of a Bendable Wing Micro-UAV for Data Collection Submitted by: AIAA Orange County Section NASA Student
PROJECT AQUILA 211 ENGINEERING DRIVE AUBURN, AL POST LAUNCH ASSESSMENT REVIEW
PROJECT AQUILA 211 ENGINEERING DRIVE AUBURN, AL 36849 POST LAUNCH ASSESSMENT REVIEW APRIL 29, 2016 Motor Specifications The team originally planned to use an Aerotech L-1520T motor and attempted four full
Preliminary Design Review November 15, Agenda. California State Polytechnic University, Pomona W. Temple Ave, Pomona, CA 91768
Preliminary Design Review November 15, 2017 Agenda California State Polytechnic University, Pomona 3801 W. Temple Ave, Pomona, CA 91768 Agenda 1.0 General Information 2.0 Launch Vehicle System Overview
AUBURN UNIVERSITY STUDENT LAUNCH. Project Nova. 211 Davis Hall AUBURN, AL Post Launch Assessment Review
AUBURN UNIVERSITY STUDENT LAUNCH Project Nova 211 Davis Hall AUBURN, AL 36849 Post Launch Assessment Review April 19, 2018 Table of Contents Table of Contents...2 List of Tables...3 Section 1: Launch Vehicle
NASA USLI Flight Readiness Review (FRR) Rensselaer Rocket Society (RRS)
2016-2017 NASA USLI Flight Readiness Review (FRR) Rensselaer Rocket Society (RRS) Rensselaer Polytechnic Institute 110 8th St Troy, NY 12180 Project Name: Andromeda Task 3.3: Roll Induction and Counter
NASA Student Launch College and University. Preliminary Design Review
2017-2018 NASA Student Launch College and University Preliminary Design Review Institution: United States Naval Academy Mailing Address: Aerospace Engineering Department United States Naval Academy ATTN:
Northwest Indian College Space Center USLI Critical Design Review
2012-2013 Northwest Indian College Space Center USLI Critical Design Review Table of Contents, Tables, and Figures I.0 CDR Report Summary... 1 I.1 Team Summary... 1 I.2 Launch Vehicle Summary... 1 I.2a
Florida A & M University. Flight Readiness Review. 11/19/2010 Preliminary Design Review
Florida A & M University Flight Readiness Review 11/19/2010 Preliminary Design Review 1 Overview Team Summary ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ ~~~~~~~~ Vehicle Criteria ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ ~~~~~~~~
NASA SL Preliminary Design Review
NASA SL Preliminary Design Review University of Alabama in Huntsville 1 Mission Summary Design, fabricate, test and fly a rocket and payload to 1 mile in altitude Deploy a rover upon landing to autonomously
Madison West High School Green Team
Madison West High School Green Team The Effect of Gravitational Forces on Arabidopsis Thaliana Development Flight Readiness Review The Vehicle Mission Performance Criteria Successful two stage flight Altitude
Critical Design Review Report NASA Student Launch Florida International University American Society of Mechanical Engineers (FIU-ASME)
Critical Design Review Report 2014-2015 NASA Student Launch Florida International University American Society of Mechanical Engineers (FIU-ASME) Florida International University Engineering Center College
USLI Flight Readiness Review
UNIVERSITY OF MINNESOTA TWIN CITIES 2011 2012 USLI Flight Readiness Review University Of Minnesota Team Artemis 3/26/2012 Flight Readiness Report prepared by University of Minnesota Team Artemis for 2011-2012
Rover Delivery NASA University Student Launch Initiative Post-Launch Assessment Review. Charger Rocket Works.
Rover Delivery 2017-2018 NASA University Student Launch Initiative Post-Launch Assessment Review Charger Rocket Works April 27 th, 2018 Propulsion Research Center 1030 John Wright Drive NW, Huntsville,
NORTHEASTERN UNIVERSITY
NORTHEASTERN UNIVERSITY POST-LAUNCH ASSESSMENT REVIEW NORTHEASTERN UNIVERSITY USLI TEAM APRIL 27TH 2018 Table of Contents 1. Summary 2 1.1 Team Summary 2 1.2 Launch Summary 2 2. Launch Vehicle Assessment
USLI Critical Design Report
UNIVERSITY OF MINNESOTA TWIN CITIES 2011 2012 USLI Critical Design Report University Of Minnesota Team Artemis 1/23/2012 Critical Design Report by University of Minnesota Team Artemis for 2011-2012 NASA
Preliminary Design Review
Preliminary Design Review November 16, 2016 11/2016 California State Polytechnic University, Pomona 3801 W Temple Ave, Pomona, CA 91768 Student Launch Competition 2016-2017 1 Agenda 1.0 General Information
CNY Rocket Team Challenge. Basics of Using RockSim 9 to Predict Altitude for the Central New York Rocket Team Challenge
CNY Rocket Team Challenge Basics of Using RockSim 9 to Predict Altitude for the Central New York Rocket Team Challenge RockSim 9 Basics 2 Table of Contents A. Introduction.p. 3 B. Designing Your Rocket.p.
Pegasus II. Tripoli Level 3 Project Documentation. Brian Wheeler
Pegasus II Tripoli Level 3 Project Documentation Brian Wheeler Contents: A. Design Overview B. Booster Construction C. Electronics Bay (Mechanical) Construction D. Nose Cone Construction E. Recovery System
NASA Student Launch W. Foothill Blvd. Glendora, CA Artemis. Deployable Rover. November 3rd, Preliminary Design Review
2017 2018 NASA Student Launch Preliminary Design Review 1000 W. Foothill Blvd. Glendora, CA 91741 Artemis Deployable Rover November 3rd, 2017 Table of Contents General Information... 9 1. School Information...
University Student Launch Initiative
University Student Launch Initiative HARDING UNIVERSITY Critical Design Review February 4, 2008 The Team Dr. Edmond Wilson Brett Keller Team Official Project Leader, Safety Officer Professor of Chemistry
University Student Launch Initiative Preliminary Design Review
UNIVERSITY OF MINNESOTA TWIN CITIES 2012 2013 University Student Launch Initiative Preliminary Design Review Department of Aerospace Engineering and Mechanics 3/18/2013 2012-2013 University of Minnesota
First Nations Launch Rocket Competition 2016
First Nations Launch Rocket Competition 2016 Competition Date April 21-22, 2016 Carthage College Kenosha, WI April 23, 2016 Richard Bong Recreational Park Kansasville, WI Meet the Team Wisconsin Space
SpaceLoft XL Sub-Orbital Launch Vehicle
SpaceLoft XL Sub-Orbital Launch Vehicle The SpaceLoft XL is UP Aerospace s workhorse space launch vehicle -- ideal for significant-size payloads and multiple, simultaneous-customer operations. SpaceLoft
The University of Toledo
The University of Toledo Project Cairo Preliminary Design Review 10/08/2016 University of Toledo UT Rocketry Club 2801 W Bancroft St. MS 105 Toledo, OH 43606 Contents 1 Summary of Preliminary Design Review...
Flight Readiness Review Report NASA Student Launch Florida International University American Society of Mechanical Engineers (FIU-ASME)
Flight Readiness Review Report 2014-2015 NASA Student Launch Florida International University American Society of Mechanical Engineers (FIU-ASME) Florida International University Engineering Center College
Post Launch Assessment Review
AIAA Orange County Section Student Launch Initiative 2011-2012 Post Launch Assessment Review Rocket Deployment of a Bendable Wing Micro-UAV for Data Collection Submitted by: AIAA Orange County Section
Pre-Flight Checklist for SLIPSTICK III
Advanced Planning 1 Schedule a Check that waivers are available at the intended launch site and date. b Check weather forecast for wind and temperature conditions at the site. c Have TAP members approved
Student Launch. Enclosed: Proposal. Submitted by: Rocket Team Project Lead: David Eilken. Submission Date: September 30, 2016
University of Evansville Student Launch Enclosed: Proposal Submitted by: 2016 2017 Rocket Team Project Lead: David Eilken Submission Date: September 30, 2016 Payload: Fragile Material Protection Submitted
Rocket Design. Tripoli Minnesota Gary Stroick. February 2010
Rocket Design Tripoli Minnesota Gary Stroick February 2010 Purpose Focus is on designing aerodynamically stable rockets not drag optimization nor construction techniques! Copyright 2010 by Gary Stroick
Project WALL-Eagle Maxi-Mav Flight Readiness Review
S A M U E L G I N N C O L L E G E O F E N G I N E E R I N G Auburn University Project WALL-Eagle Maxi-Mav Flight Readiness Review 2 Engineering Dr. Auburn, AL 36849 March 6th, 205 Table of Contents Section
Rocketry Projects Conducted at the University of Cincinnati
Rocketry Projects Conducted at the University of Cincinnati 2009-2010 Grant Schaffner, Ph.D. (Advisor) Rob Charvat (Student) 17 September 2010 1 Spacecraft Design Course Objectives Students gain experience
NWIC Space Center s 2017 First Nations Launch Achievements
NWIC Space Center s 2017 First Nations Launch Achievements On April 18, 2017, we were on two airplanes to Milwaukee, Wisconsin by 6:30 am for a long flight. There were 12 students, 3 mentors, 2 toddlers
Northwest Indian College Space Center USLI Post Launch Assessment Review
Northwest Indian College Space Center USLI Post Launch Assessment Review 2012-2013 Table of Contents I. Team Summary... 1 Team Name: Northwest Indian College RPGs... 1 II. Launch Vehicle Summary... 1
ISS Space Grant Team Exocoetidae
ISS Space Grant Team Exocoetidae Illinois Space Society University of Illinois at Champaign-Urbana March 9, 2018 Faculty Advisor: Diane Jeffers (dejeffer@illinois.edu, 217-898-5888) Team Lead: Shivani
LEVEL 3 BUILD YELLOW BIRD. Dan Schwartz
LEVEL 3 BUILD YELLOW BIRD Dan Schwartz This entire rocket is built using the same techniques I use for my nose cones, a central airframe tube for compression strength and rings of high compression styrofoam
Cal Poly Pomona Rocketry NASA Student Launch Competition POST LAUNCH ASSESMENT REVIEW April 24, 2017
Cal Poly Pomona Rocketry NASA Student Launch Competition 2016-2017 POST LAUNCH ASSESMENT REVIEW April 24, 2017 California State Polytechnic University, Pomona 3801 W Temple Ave, Pomona, CA 91768 Department
AKRONAUTS. P o s t - L a u n c h A ss e s m e n t R e v i e w. The University of Akron College of Engineering. Akron, OH 44325
AKRONAUTS Rocket Design Team Project P o s t - L a u n c h A ss e s m e n t R e v i e w The University of Akron College of Engineering 302 E Buchtel Ave Akron, OH 44325 NASA Student Launch Initiative April
Innovating the future of disaster relief
Innovating the future of disaster relief American Helicopter Society International 33rd Annual Student Design Competition Graduate Student Team Submission VEHICLE OVERVIEW FOUR VIEW DRAWING INTERNAL COMPONENTS
Project WALL-Eagle Maxi-Mav Critical Design Review
S A M U E L G I N N C O L L E G E O F E N G I N E E R I N G Auburn University Project WALL-Eagle Maxi-Mav Critical Design Review 2 Engineering Dr. Auburn, AL 36849 January 6th, 205 Table of Contents SECTION
Critical Design Review
Harding University University Student Launch Initiative Team Critical Design Review January 29, 2007 The Flying Bison Sarah Christensen Project Leader Dr. Ed Wilson Faculty Supervisor Dr. James Mackey
THE UNIVERSITY OF AKRON
THE UNIVERSITY OF AKRON College of Engineering 302 E Buchtel Ave Akron, OH 44325 September 20, 2017 NASA Student Launch Initiative Table of Contents 1. Adult Educators and Advisors... 4 2. Team Officials...
UC Berkeley Space Technologies and Rocketry NASA Student Launch Proposal Project Arktos. 432 Eshleman Hall, MC 4500 Berkeley, CA
UC Berkeley Space Technologies and Rocketry NASA Student Launch Proposal Project Arktos 432 Eshleman Hall, MC 4500 Berkeley, CA 94720-4500 September 20, 2017 Contents 1 General Team Information 3 1.1 Key
Post Launch Assessment Review
Post Launch Assessment Review University of South Alabama Launch Society Conner Denton, John Faulk, Nghia Huynh, Kent Lino, Phillip Ruschmyer, Andrew Tindell Department of Mechanical Engineering 150 Jaguar
York College of Pennsylvania NASA Student Launch Preliminary Design Report
York College of Pennsylvania NASA Student Launch 2017-2018 Preliminary Design Report The Aurora Project 441 Country Club Road York, PA 17403 1 General Information Contact Information: Campus Leader: YCP
267 Snell Engineering Northeastern University Boston, MA 02115
NUMAV 267 Snell Engineering Northeastern University Boston, MA 02115 Mentor Robert DeHate President, AMW/ProX NAR L3CC 75198 TRA TAP 9956 robert@amwprox.com (978)766-9271 1 Table of Contents 1. Summary.3
By: Georgia Institute of Technology Team Autonomous Rocket Equipment System (A.R.E.S.) Georgia Institute of Technology North Avenue NW Atlanta GA,
By: Georgia Institute of Technology Team Autonomous Rocket Equipment System (A.R.E.S.) Georgia Institute of Technology North Avenue NW Atlanta GA, 30332 Project Name: Hermes MAXI-MAV Competition Friday,
Table of Content 1) General Information ) Summary of PDR Report ) Changes Made Since Proposal ) Safety... 8
Table of Content 1) General Information... 3 1.1 Student Leader... 3 1.2 Safety Officer... 3 1.3 Team Structure... 3 1.4 NAR/TRA Sections... 4 2) Summary of PDR Report... 5 2.1 Team Summary... 5 2.2 Launch
University of North Dakota Department of Physics Frozen Fury Rocketry Team
University of North Dakota Department of Physics Frozen Fury Rocketry Team NASA Student Launch Initiative Flight Readiness Review - Report Submitted by: The University of North Dakota Frozen Fury Rocketry
Tuskegee University Rocketry Club
Tuskegee University Rocketry Club National Aeronautics and Space Administration Student Launch Initiative Preliminary Design Review Atmospheric Measurement and Aerodynamic Analysis TURC 2015-2016 NASA
Cornell Rocketry Team. NASA Student Launch Competition CORNELL ROCKETRY TEAM
2015-2016 CORNELL ROCKETRY TEAM Presentation Centennial Challenge MAV Participant NASA Student Launch Competition LAUNCH VEHICLE GENERAL DIMENSIONS Airframe Tubing: OD = 3.98 in ID = 3.9 in Couplers: OD
Pre-Launch Procedures
Pre-Launch Procedures Integration and test phase This phase of operations takes place about 3 months before launch, at the TsSKB-Progress factory in Samara, where Foton and its launch vehicle are built.
CYCLONE STUDENT LAUNCH INITIATIVE
NSL PROPOSAL September 19, 2018 CYCLONE STUDENT LAUNCH INITIATIVE 2018-19 Iowa State University 537 Bissell Rd. 1200 Howe Hall Ames, IA 50011 Table of Contents Table of Contents... 2 Table of Figures...
Reentry Demonstration Plan of Flare-type Membrane Aeroshell for Atmospheric Entry Vehicle using a Sounding Rocket
AIAA ADS Conference 2011 in Dublin 1 Reentry Demonstration Plan of Flare-type Membrane Aeroshell for Atmospheric Entry Vehicle using a Sounding Rocket Kazuhiko Yamada, Takashi Abe (JAXA/ISAS) Kojiro Suzuki
Team 65 Project Technical Report to the 2018 Spaceport America Cup
Team 65 Project Technical Report to the 2018 Spaceport America Cup 1 Matt Valenzeno University of Illinois at Chicago, Chicago, Illinois, 60607 2 Rachel Cruz University of Illinois at Chicago, Chicago,
What s New in Designing for Helicopter Duration
What s New in Designing for Helicopter Duration Prepared for NARCON-2017 Chris Flanigan NAR 17540 L1 1 Topics Quick review of theory Blade design & airfoil selection Hub construction Internal or external
THE FALCON I LAUNCH VEHICLE Making Access to Space More Affordable, Reliable and Pleasant
18 th Annual AIAA/USU Conference on Small Satellites SSC04-X-7 THE FALCON I LAUNCH VEHICLE Making Access to Space More Affordable, Reliable and Pleasant Hans Koenigsmann, Elon Musk, Gwynne Shotwell, Anne