PPT-Launch Vehicle Liftoff Vibroacoustics

Revision A By Tom Irvine Vibrationdata Vibrationdata Space Shuttle Liftoff Environments Water Supply Tank Adjacent to Launch Pad The ignition of the Space Shuttles three main engines followed by the ignition of the twin solid rocket boosters generated the thrust necessary for the Space Shuttle liftoff. ORS 803112 BUYER If you do not apply for a title within 30 days from the date of purchase you may be subject to a late title transfer fee The information on this form is collected under the authority of the Motor Vehicle Act Section 216 The information will be us ed to process your vehicle inspection If you have any questions please call 2509520577 or see our website at wwwthgovbccacv @arianespace 1 LV Liftoff 2 3 First Burn into Parking Orbit 4 Second Burn into Intermediate Orbit 5 Third Burn and APT Jettison 6 Fourth Burn into Transfer Orbit 7 Fifth Burn into Geosynchronous Transfer Orbi Preliminary Design Review. Rocket & Payload Schematic. Lift Off. Apogee and ejection of drogue parachute. Payload and main chute deployment. Trajectory of Rocket . Rocksim predicted trajectory of rocket. CDR Presentation. 2015-2016. AXIOM . Overview . Launch Vehicle Design. Dimensions. Stability. Propulsions. Avionics. Recovery System. Payload Bay Integration. Subscale Manufacturing . Subscale Data. AGSE Design. Preliminary Design . Review Presentation. Launch Vehicle Dimensions. Size and mass. Length: 110”. Diameter: 5.5”. Mass Without Motor: 236.36 oz. Mass With Motor: 311.44 oz. Stability Margin. CP (from nose): 77.03 in.. Alabama Rocket Engineering Systems (ARES) Team. The University of Alabama. Overview. Mission Overview. Team Introduction. Launch Vehicle Design. Payload Design. Project Plan. Q & A. Mission Overview. University of New Hampshire Rocket Cats. Collin Huston, Brian Gray, Joe Paulo, Shane Hedlund, . Sheldon McKinley, Fred . Meissner. , Cameron Borgal. 2012-2013 Flight Readiness Review. Submission Deadline: March 18, 2013. Process. EE290G. Joey . Greenspun. An SOI Process For Fabrication of Solar Cells, Transistors and Electrostatic Actuators. Power, computation, actuation. Process geared towards creation of . microrobots. Based on the flight-proven Athena I & II, these vehicles are designed to provide reliable access to space for small payloads, to a wide range of orbits. . The Athena launch vehicle family combines both companies’ heritage and expertise to provide reliable launch services at an affordable price. . Mission Concept 1. Open Issues. Face-to-Face . #5. June . 1-2, 2017. Ruth.C.Carter@nasa.gov. 1. . 1. Concept 1 Design Status/Issues. Concept 1 mass is . ~. 2. ,000 kg over the launch vehicle (Vulcan Aces 5m fairing) lift capability . Presented to the Review of U.S. Human Spaceflight Plans Committee . June 17, 2009. 1. 1990’s NASA sponsored Shuttle C. Side-Mount Shuttle Derived Vehicle Concepts. Have Matured Via Several Major Design Studies. Vehicle dimensions, materials, and justifications. Static stability margin. Plan for vehicle safety verification and testing. Baseline motor selection and justification. Thrust-to-weight ratio and rail exit velocity.