html5-img
1 / 18

Dorrie Byford Week 7: March 1 st , 2007

Dorrie Byford Week 7: March 1 st , 2007. Communications Group Leader / Autonomous Rendezvous / Integration Team / Website Designer Dish Diameter, Power, Mass, and Volume for all Vehicles and Satellites. Highlights of Analysis. Transfer Vehicle 1 x 4.75 m dish, 1 x 1.5 m dish

dane-neal
Download Presentation

Dorrie Byford Week 7: March 1 st , 2007

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. Dorrie ByfordWeek 7: March 1st, 2007 Communications Group Leader / Autonomous Rendezvous / Integration Team / Website Designer Dish Diameter, Power, Mass, and Volume for all Vehicles and Satellites Dorrie Byford

  2. Highlights of Analysis • Transfer Vehicle • 1 x 4.75 m dish, 1 x 1.5 m dish • 14.25 kW + 1.25 kW = 15.5 kW • .25 mt + .15 mt = .4 mt • Earth Taxi / Mars Taxi • 1 m dish x2 • 1 kW x2 • .15 mt x2 • All Other Space Traveling Vehicles • 1.5 m dish x2 • 1.25 kW x2 • .15 mt x2 Dorrie Byford

  3. IMLEO / IVLEO • Comm Satellites • 2.74 mt • 123.49 m^3 (stowed) • GPS Satellites • 1.74 mt • 55.32 m^3 (stowed) • Sat totals: • Power: 44 kW • Mass: 18 mt • Volume: 730 m^3 CAD by: Steve Kassab Dorrie Byford

  4. Back-up Slides Dorrie Byford

  5. Link Budget Analysis • A budget analysis was performed for every vehicle to ensure complete coverage during the entire mission. Power and dish size were optimized by increasing transmission time. A table of maximum transmission times can be found on the next slide. Link budget analysis for each vehicle follows. Dorrie Byford

  6. Dorrie Byford Comm Spreadsheet *Could not get TC traj dimensions from Chris Bush in time. Dorrie Byford

  7. Info on Comm Data Sheet • Video • Traveling Vehicles • Transfer Vehicle • Since the crew will be in the Transfer Vehicle the most, I allotted one video feed per crew member plus one in the common area. This high HD video requirement is what drove up the power estimates and dish size. • Taxi Capsule • The crew spends very little time in this vehicle, and it is very small, so only one video feed was allotted. Also, because of the vehicle’s constant proximity to a planet, the power requirements and dish size remain low (not much distance to transmit over). Dorrie Byford

  8. Info on Comm Data Sheet (cont) • Video • Mars Vehicles / Structures • All vehicles and structures on Mars require very little power. This is because the satellites in Mars-stationary orbit are only 20,462 km away. • These structures and vehicles also will not require a satellite dish. Instead they will have a transmission antenna similar to that on an aircraft. Dorrie Byford

  9. Info on Comm Data Sheet (cont) • Diameter • Traveling Vehicles • Vehicles Requiring Video • The Transfer Vehicle and Taxi Capsule require video to meet mission requirements. The diameters of the TV dish is the largest because it has the most data to transmit over the farthest distance. The TC dish is still small in size because of its proximity to the planet. • The TV also has a smaller antenna for voice/data/telemetry/commanding. This serves as an emergency communication system. The TV will always be able to transmit directly back to Earth using this dish (does not need to be bounced off of any satellites unless there is no line of sight). Dorrie Byford

  10. Info on Comm Data Sheet (cont) • Diameter • Traveling Vehicles • Vehicles Not Requiring Video • These vehicles are equipped with a dish to allow for data/telemetry/commanding. There will be two identical dishes on each vehicle; one as prime and one as back-up. The second will require little power (only thermal) since it will not nominally be in operation. Dorrie Byford

  11. Info on Comm Data Sheet (cont) • Power • All power requirements were derived using the Link Budget Analysis found in future slides. • Mass/Volume • Mass and volume, where applicable, were estimated by finding a trend in historical data (see future slides). A value of “<<“ means that the value is so small (< .01 mt for mass) that the number is negligible. For volumes with a “<<“, the dish will be stored inside the vehicle, thus not adding to the IVLEO. Dorrie Byford

  12. Info on Comm Data Sheet (cont) • Percentage • Transfer Vehicle • For the TV, the percentage indicates at what point the vehicle changes from transmitting to Earth to transmitting to the Gangale sats. When the TV departs Earth, for the first 75% (distance) of the trip, all communication is sent back to Earth and then forward to Mars and other vehicles, if necessary. At the 75% point, all comm is sent through the Gangale sats and then bounced back to Earth. This is necessary to reduce the size and power requirement of the dish on the vehicle. • Other Vehicles and TV Back-up Comm System • The other vehicles and the TV’s back-up comm system with values of 100/38 can communicate directly to Earth 100% of the trip, but can communicate directly to the Gangale sats only during the last 38% of the trip. • These percentages are what drive the max transmit time for each vehicle (seen in previous slide). Dorrie Byford

  13. Transfer Vehicle Earth to 75% of Total Distance 75% Distance to Mars Dorrie Byford

  14. TV Back-up & Other Traveling Vehicles Dorrie Byford

  15. Satellite Info • This table was used to create the estimates for the satellite’s masses and volumes. (see following graphs) Dorrie Byford

  16. Graph to Estimate Sat Mass Dorrie Byford

  17. Graph to Estimate Sat Volume Dorrie Byford

  18. References • http://www.boeing.com/defense-space/space/bss/programs.html • http://science.ksc.nasa.gov/shuttle/technology/sts-newsref/sts-jsc-comm.html Dorrie Byford

More Related