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DeviceNet FBM229

DeviceNet FBM229

DeviceNet FBM229. Thad Frost. Agenda. DeviceNet Agenda. 1. What is DeviceNet?. 2. Overview of the Invensys Solution . 3. Physical Layer. 4. Supporting Software. 5. Release Information and Certification. 6. Competitive Information. 7. FAQ. 8. Demo. What is DeviceNet?.

By daxia
(477 views)

VII. Aerocapture System Technology for Planetary Missions

VII. Aerocapture System Technology for Planetary Missions

VII. Aerocapture System Technology for Planetary Missions. Session Facilitator: Michelle Munk. Presentation to NMP ST9 Workshop Washington, D.C. February 2003. Outline. Executive Summary Aerocapture Capabilities to be Validated by ST9 Aerocapture Overview

By daisy
(127 views)

MAT Code

MAT Code

Danielle Yaple 7 February 2008 Avionics Group, GC, CAD, MAT M odel A nalysis T rios Combined Code. MAT Code. User Inputs Delta V (vary case to case, 7000,9000,12000,15000,18000 m/s) Payload Mass (.2, 1, 5 kg) Stages (2 or 3) Propellant Type (Cryogenic, Storable , Hybrid , or Solid)

By martha
(148 views)

Low Energy Interplanetary Transfers Using the Halo Orbit Hopping Method with STK/Astrogator

Low Energy Interplanetary Transfers Using the Halo Orbit Hopping Method with STK/Astrogator

Low Energy Interplanetary Transfers Using the Halo Orbit Hopping Method with STK/Astrogator. Tapan R. Kulkarni Daniele Mortari Department of Aerospace Engineering, Texas A&M University College Station, TX 77840. Outline. Aims and Scope of this research

By dexter
(115 views)

Slawomir Boruch Week 3: February 1 st , 2007

Slawomir Boruch Week 3: February 1 st , 2007

Slawomir Boruch Week 3: February 1 st , 2007. Dynamics & Control EP Trajectory Design, aM, aE, EPS1, EPS2, Sample Return vehicle groups. Future Work. Work needs to be checked via numerical integration Should consider 3-D case (inclinations) Unknown masses major source of error.

By ken
(106 views)

Thermal Control

Thermal Control

Thermal Control. Impact Boom Stowed and Deployed SWEA STE Magnetometer. Bob Eby Swales Aerospace. BEBY@SWALES.COM. R.Eby. IMPACT BOOM STOWED. Housing for boom & release mechanism covered with MLI Conductively isolated from S/C, R= 25 C/W

By azia
(125 views)

Week 4 Presentation Thursday, Feb 5, 2009

Week 4 Presentation Thursday, Feb 5, 2009

Orbit Transfer Vehicle Electric Propulsion System: High-Level Analysis and Component Specifications. Week 4 Presentation Thursday, Feb 5, 2009. 1. Electric Propulsion System Analysis. Determine a performance range for mission feasibility Choose a thruster for the X1 design

By vala
(81 views)


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