'Delta v' presentation slideshows

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?.

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

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)

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

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.

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

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