Www.nasa.gov Ares I-X Status July 30, 2009. Ares I-X Flight Test Overview  Ares I-X is a Constellation Program developmental flight test for the Ares.

Slides:



Advertisements
Similar presentations
January 22, 2009 Ares I-X Crew Module and Launch Abort System (CM/LAS) Jonathan Cruz Deputy Project Manager Jonathan Cruz Deputy Project Manager.
Advertisements

UF Hybrid Rocket Teams Mile High Club Brought to you by Chris Leonard, Ty Morton, Alex Aueron, Sam Darr, and Josh Childs.
National Aeronautics and Space Administration Presentation to the NASA Goddard Academy 2. Constellation Overview Ken Davidian Lead, Commercial.
Northwestern University Space Technology and Rocketry Society (NUSTARS) NASA Student Launch Flight Readiness Review March 16, 2015.
Vibrationdata 1 Unit 8 Waterfall FFT. Vibrationdata 2 Terrier Black Brant The Terrier-Black Brant is a two-stage, solid propellant, rail launched, guided,
Blue Origin AIAA Civil Space Symposium Huntsville, Alabama
Ares V RFI Point of Departure Information Package
Solid Rocket Boosters Overview Two solid rocket boosters provide the main thrust to lift the Space Shuttle off the pad. They are the largest solid- propellant.
Critical Design Review NASA University Student Launch Initiative University of Nebraska–Lincoln
Illinois Space Society Tech Team USLI CDR Presentation.
System Identification of a Nanosatellite Structure Craig L. Stevens, Jana L. Schwartz, and Christopher D. Hall Aerospace and Ocean Engineering Virginia.
National Aeronautics and Space Administration 1 GRC All-Hands Meeting 1 May 2006.
National Aeronautics and Space Administration DEVELOP National Program 2.
ME 501 Corey Roberts Leo Montgomery Motor Plate Analysis.
National Aeronautics and Space Administration Explorers’ Guide to the Solar System 1 National Aeronautics and Space Administration
Critical Design Review of “Mach Shock Reduction” Phase II January 2008 Statesville, NC.
Illinois Space Society Tech Team USLI FRR Presentation.
Intercollegiate Rocket Engineering Competition Spring 2015 EML Ethics and Design Project Organization.
CONSTELLATION National Aeronautics and Space Administration Ares Project Overview – Quality in Design Chris Cianciola Kenneth Crane.
National Aeronautics and Space Administration General ICD information for SDRs For consideration for EDS Development Sandra Johnson NASA Glenn.
Science Fiction. Rocket flight Centre of Mass or Centre of Gravity (CM or CG) Centre of mass is the mean or central location of all the mass of an object.
A3 Altitude Test Facility
1 Aeronautics Explorer Post Katherine ‘Katie’ Fallon Midview HS Goal: Aeronautics Explorer Post Katherine ‘Katie’ Fallon Midview HS Goal:To explorer the.
Requirements and Operations Team Industry Day Briefing 17 January, 2002.
National Aeronautics and Space Administration Checklists and Testing Systems.
University of Florida Rocket Team Critical Design Review Presentation.
Critical Design Review Presentation Jan. 20, 2011.
Rockets Applied Science Fall 08 Mrs. Dickerson.
1 Commercial Crew Program The Next Step in U.S. Space Transportation Brent W. Jett October 11, 2012 Commercial Crew Program - Same Crew…New Ride.
Ares I-X INDUSTRY DAY Scott Graham William Foster Monica Hoffmann
HARDING UNIVERSITY A Study of Atmospheric Properties as a Function of Altitude Flying Bison.
PROGRAM UPDATE March 2012.
AAE 450- Propulsion LV Stephen Hanna Critical Design Review 02/27/01.
National Aeronautics and Space Administration Transitioning Toward the Future of Commercial Human Spaceflight COMMERCIAL CREW PROGRAM AIAA Spring Dinner.
Preliminary Design Review.  Completed practice launch  New motor selection  Corrected simulations  Improved payload construction  Increased.
High Altitude Balloon Michael Adams Alex Fletcher Jon Welch.
Human Exploration of Mars Design Reference Architecture 5
D EPARTMENT OF M ECHANICAL AND A EROSPACE E NGINEERING HIGH POWERED ROCKETRY CLUB PDR PRESENTATION 1.
National Aeronautics and Space Administration Ares Project Joel Best / EO10 November 6, 2006 Ares Project Joel Best / EO10 November 6, 2006.
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 Critical Design Review 15 Janurary2015 Northwestern University | 2145 Sheridan Road | Evanston, IL
Bernadette Cannon Daniel Roh Daniel Du. Design Team America Rocketry Challenge’s goal is to get a model rocket to fly to a height of exactly 825 feet.
Launch Structure Challenge - Background Humans landed on the moon in 1969 – Apollo 11 space flight. In 2003, NASA started a new program (Ares) to send.
Flight Hardware. Flight Profile - STS Flight Profile - SLS Earth Mars 34,600,000 mi International Space Station 220 mi Near-Earth Asteroid ~3,100,000.
UCF_USLI Preliminary Design Review David Cousin Freya Ford Md Arif Drew Dieckmann Stephen Hirst Mitra Mossaddad University of Central Florida.
How Astronauts Got Launched to the Moon Created by: Luke Sharman.
High Altitude Rocket Project School of Science and Engineering | Integrated Project Mjölnir.
Spaceports – Emerging Business Models
* 07/16/96 Propulsion Lab 6 Winter Quarter *.
2018 First Nation Launch - Flight Readiness Review
3/21/2017 A Couplings Approach to Mitigate Unexpected Behaviors in Large Scale Complex Engineering Systems Ben Giles Mentor: Dr. Christina Bloebaum.
Space Travel Present & Future
North Dakota Space Grant Consortium
Ares I System Requirements Review (SRR)
Ares Project Overview – Quality in Design
System Identification of a Nanosatellite Structure
Final Readiness Review
Mars as Seen from Phobos
2019 First Nation Launch – FRR Virtual Review
2019 First Nation Launch – PDR Virtual Review
International Space Station Providers
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)
2019 First Nation Launch – Oral Presentation
2019 First Nation Launch – CDR Virtual Review
University of Iowa USLI
2019 First Nation Launch – Oral Presentation
Presentation transcript:

Ares I-X Status July 30, 2009

Ares I-X Flight Test Overview  Ares I-X is a Constellation Program developmental flight test for the Ares I project There are five primary flight test objectives – P1 through P5 Ares I-X is an un-crewed suborbital test Flight Test Profile P2) Perform in-flight separation/staging ~130,000 feet P5) Characterize integrated vehicle roll torque ~150,000 feet P4) Demonstrate first stage entry dynamics and post staging sequencing of events (e.g. employ booster tumble motors and deploy parachutes) First Stage recovery P1) Demonstrate controllability P3) Demonstrate assembly and recovery of an Ares I similar first stage Upper Stage/ Crew Module/ Launch Abort System Simulator free fall into ocean Vehicle Height:327 feet Weight at Ignition:1.8 M-lbm Max. Acceleration:2.5 g Max. Speed:Mach 4.8 National Aeronautics and Space Administration 2

Orion Crew Module/ Launch Abort System (CM/LAS) Simulator 4/096/09 National Aeronautics and Space Administration 3

Upper Stage Simulator (USS) National Aeronautics and Space Administration 4 6/09 7/09

Roll Control System (RoCS) National Aeronautics and Space Administration 5 4/09

First Stage National Aeronautics and Space Administration 7/09

Avionics National Aeronautics and Space Administration 7 7/09 5/09

Vehicle Assembly Building (VAB) Operations National Aeronautics and Space Administration 8 artist concept 5/09

Modal Testing National Aeronautics and Space Administration 9 5/09

Stack 0 National Aeronautics and Space Administration 10

Stack 1 National Aeronautics and Space Administration 11

Stack 2 National Aeronautics and Space Administration 12 artist concept

Stack 3 National Aeronautics and Space Administration 13 artist concept

Stack 4 National Aeronautics and Space Administration 14 artist concept

Stack 5 National Aeronautics and Space Administration 15 artist concept

Integrated Vehicle National Aeronautics and Space Administration 16 artist concept