'Payload' diaporamas de présentation

Chapter 5 Helicopter Performance. SONG, Jianyu . What Can We Learn?. Performance: estimation of required power maximum level flight speed endurance range …. The International Standard Atmosphere. The International Standard Atmosphere (ISA) .

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.

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

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.

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:

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.

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.

COMP514 – Advanced Communications. Lecture 2: SDH Matthew Luckie mluckie@cs.waikato.ac.nz. Lecture Outline. SDH : Synchronous digital hierarchy Self-healing rings OAM Fault location. Synchronous Digital Hierarchy (SDH). Dominant standard for digital telecommunications networks. STM-1.

HIGH SPEED OHE OF INDIAN RAILWAYS. ISSUES CHALLENGES OPTIONS. Presented by – J. N. LAL SENIOR EXECUTIVE DIRECTOR (TRACTION INSTALLATION). RESEARCH DESIGNS AND STANDARDS ORGANISATION. INTRODUCTION. RESEARCH DESIGNS AND STANDARDS ORGANISATION. RAILWAY SYSTEM. ENERGY EFFICIENT

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.

Traffic Generator. Transmits UDP packets (packet format on the next slide) 5 words liquid app header 1000 Bytes payload Note: A word might be split across two packets! Payload is ASCII text Can be from a file Default file is "data“ (“tempest” Shakespeare play – 99,379 Bytes).

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 :.

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

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.

Pre-Burst Chaos. Howard L. Brooks Dept. of Physics and Astronomy DePauw University Greencastle, Indiana hlbrooks@depauw.edu www.depauw.edu/acad/physics/base. Indiana Space & Earth Workshop Flight 12 Nov.2009 video. 72,000’ first wind sheer 76,000’ Payloads are stable

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.

Guidelines for Using SDL in Product Development. Frank Weil Motorola Global Software Group – Software Design Automation. Overview. General Recommendations for Design Models Recommendations on SDL Usage for Design Performance Considerations Platform Interfaces Portability Issues

ANITA-lite: The Background Survey. Jim Beatty Penn State. Context. A simple ‘Pathfinder’ program has been under consideration for some time to map the polar winds using small inexpensive payloads Iridium plus GPS ‘Antarctic sondes’

RezRiders. Mission statement. Through the USLI program the Northwest Indian College Space Center’s RezRiders Team enhances its involvement in science, math, engineering and technology and encourages others in Tribal communities to do the same.

MAGGEX. Post-Flight Analysis. Magnetic Field Overview. B=B m +B c +B d B m : Earth’s fluid conducting outer core 95% of measured field B c : Magnetized rocks in crust (~.02 mG) B d : Currents induced in magnetosphere by solar and extraterrestrial activity (~.250mG)