'Payload' diaporamas de présentation

Quarterly Business Partner Meeting

Quarterly Business Partner Meeting . Tuesday, July 13 th 2010 Dial-in Info: 888-288-9321 Passcode: 548317. Your lines will be muted, however we will open them at the end for Q&A.

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Chapter 5 Helicopter Performance

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HIGH SPEED OHE OF INDIAN RAILWAYS

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Pre-Burst Chaos

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RezRiders

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Guidelines for Using SDL in Product Development

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GPS Vehicle Tracking/Payload Release System For Small UAV

GPS Vehicle Tracking/Payload Release System For Small UAV. Project Team 02009. Project Summary. Motivation for the Project Objectives: Accurate Tracking of a UAV Wireless Data Transmission Autonomous Function : Drop a Payload. Project Requirements.

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19 Mile High Club

19 Mile High Club. High Altitude Balloon Michael Adams Alex Fletcher Jon Welch. Objective. Achieve 100,000 feet Freefall to 60,000 feet Deploy Parachute Arrested Fall Collect data along the way. Basic Set-Up. Background.

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21 - Interstellar Spaceflight

21 - Interstellar Spaceflight. THE PHYSICS OF SPACE TRAVEL (AS WE UNDERSTAND IT). For a spacecraft accelerating at a rate a , the velocity v reached and distance x traveled in a given interval of time t is:. c = speed of light. Accelerating at 1g = 9.8 m/s 2 :.

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ANITA-lite: The Background Survey

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Embry-Riddle Aeronautical University ASCEND! Payload

Embry-Riddle Aeronautical University ASCEND! Payload. Fall 2013 ERAU NASA Space Grant. ASCEND Team. Robert Bearden Dallas Hodge Aaron Petreck Ryan Sallee Clayton Jacobs Kevin Jordan Mo Sabliny. Outline. Payload Structure Components Specifications of components Software

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Operationally Responsive Space Briefing to Commercial Space Transportation Advisory Committee

Operationally Responsive Space Briefing to Commercial Space Transportation Advisory Committee 21 May 2009. Dr. Peter Wegner Director, ORS Office. Operationally Responsive Space: Four Reasons, One ORS, One Mission. Space Protection, robust space capabilities.

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System F6

http://www.darpa.mil/tto/programs/systemf6/Briefings/Overview.pptx http://www.darpa.mil/tto/programs/systemf6/index.html. System F6. Paul Eremenko Tactical Technology Office Defense Advanced Research Projects Agency (571) 214-2436 paul.eremenko@darpa.mil February 2010.

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Team B.O.D.

Team B.O.D. Francesca Johnson Matthew Hobden Mike Davis. Mentors: Dr. Tim Frank Rick Sparber. Payload. Weight 14 oz. GPS Subsystem (BRB) Canon Firmware Hacked. Hacked - Canon. Installed Firmware Hack (CHDK) Still images every 20 seconds. Tracking the Payload. GPS Transmitter:

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MAGGEX

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Heavy IMC end payload requirements

Heavy IMC end payload requirements. M.Punturo. Translation of the IMC end mirror. Current payload is made in such a way the suspension point can be translated by 11cm in the beam axis direction. Motorization. Counter-weight (800g). 360g mirror and ~5kg reference mass.

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Non-Ionizing Radiation

Non-Ionizing Radiation. An electro-magnetic wave that has insufficient energy/quanta ( typically <10-34eV) to remove electrons from an atom. Electro-magnetic Spectrum. Types, affects and typical sources. Typical flight project sources:. S/C Transmitters

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HY-1B Payload

HY-1B Payload. 1. COCTS - Chinese Ocean Color and Temperature Scanner by SITP 2. CZI - Coastal Zone Imager (CCD Cameral) by CAST. HY-1B. Major parameters of COCTS and CZI. COCTS bands and detection object. CZI bands and detection object.

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Traffic Generator

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