AAE450 Spring 2009 Ground Stations All Phases and Payloads Trenten Muller March 5, 2009 [Trenten Muller] [COM]

Slides:

Advertisements

Similar presentations

MALAWI COAL TO POWER MALAWI GROWTH Malawi Trade & Investment Forum March 2013.

Advertisements

BA 275 Quantitative Business Methods

AAE450 Spring 2009 Hopper Trajectory February 26, 2009 [Alex Whiteman] [Mission Ops] [Lunar Descent] Page 1.

AAE450 Spring 2009 Slide 1 of 8 Orbital Transfer Vehicle (OTV) Masses and Costs Ian Meginnis March 12, 2009 Group Leader - Power Systems Phase Leader -

AAE450 Spring 2009 Analysis of Trans-Lunar Spiral Trajectory [Levi Brown] [Mission Ops] February 12,

AAE450 Spring 2009 Final Sizing and Trajectory Design for 100 g/10kg Payloads [Levi Brown] [Mission Ops] March 12,

AAE450 Spring 2009 Week 4 Presentations [Solomon Westerman][PM]

AAE450 Spring 2009 Project X pedition Final slides outline for Orbital Transfer Vehicle Propulsion Week 11 Presentation Thursday, March 26, 2009 Brad Appel.

AAE450 Spring 2009 Tony Cofer Power Group TLI Phase 03/05/09 Power Limitations for Arbitrary Payload Tony Cofer] [Power] page 1.

AAE450 Spring 2009 Descent Trajectory Hover Trajectory LD Code Integration John Aitchison March 5 th, 2009 [John Aitchison] [Mission Ops]

AAE450 Spring 2009 Lunar Capture Altitude Mass to LLO for Arbitrary Time to Rotate Lander During Descent Camera/Dust Removal [Kara Akgulian] [Mission Ops]

AAE450 Spring 2009 Hopper Design Alternative Josh Lukasak Attitude Group Lead Lunar Decent Phase Lead 02/26/09 [Josh Lukasak] [Attitude] (1)

AAE450 Spring 2009 X 0 Power System Solar - Battery Solar arrays Tony Cofer- Power System.

AAE450 Spring 2009 Launch Vehicle Performance Payload Cannon Zarinah Blockton Mission Ops~Group Earth to LEO~Phase Rover ~Phase February 19, 2009.

AAE450 Spring 2009 Patch Antenna Pivot Michael Christopher -Communications Group -TLI Phase Group 1 OF 5Michael Christopher - COM.

AAE450 Spring 2009 Communications Equipment Horizontal crash Trenten Muller Feb. 19, 2009 [Trenten Muller] [COM]

AAE 450 Spring 2008 Jeffrey Stuart January 17, 2008 Dynamics and Control Initial Inertia Matrix and Launch Scenario Considerations.

AAE 450 Spring 2008 Allen Guzik January 31, 2008 Trajectory Airplane Launch Trajectory Code and ΔV Drag Comparison Trajectory Optimization 1/5.

AAE 450 Spring 2008 Justin M. Rhodes Avionics – Telecommunications Webmaster Telecommunications and Wiring.

AAE 450 Spring 2008 Jerald A. Balta 3/27/2008 Propulsion Team/CAD Final Slides.

Phase Difference = Phase Difference = 0.05.

Link Loss  What is Link Loss? P t (transmitted power) – P r (received power) P t (transmitted power) – P r (received power)  Why calculating link loss?

Example: a radio station on the surface of the earth radiates a sinusoidal wave with an average total power of 50 kW.* Assuming the wave is radiated equally.

Injection / Withdrawal Transmission Cost Allocation Updated Slides OMS CARP Group November 19, 2009.

AAE 450 Spring 2008 Stephanie Morris 3/27/08 Propulsion Final Slides.

AAE450 Spring 2009 BAE Single Board Computer Ground Based Systems Communications Group Trans Lunar Phase Group Joshua Elmshaeuser Communications 1.

AAE450 Spring 2009 Launch Vehicles Zarinah Blockton Mission Operations 1/29/2009 Blockton Ops.

16 世纪～ 17 世纪初，出了一位是丹麦的观测家第谷，他是个超群出众的观测家，他用自制的精确仪器辛勤地观测了 20 年，取得了关于行星运动的大量数据。（ 1546 ～ 1601 ）第谷.

Ecosystems and Biomes A Voyage to Mars. Objectives The student will be able to: Describe the position of each planet with respect to the sun Explain why.

AAE450 Spring 2009 Communications Ground Stations Communication Equipment Alternative Landing Method March 26, 2009 [Trent Muller] [COM]

Celestial Sphere. Earthly Sphere Latitude measures the number of degrees north or south of the equator. –DeKalb at 41° 55’ N Longitude measures degrees.

AAE 450 Spring 2008 William Yeong Liang Ling 1/31/2008 Propulsion Cost Model of Balloon and Aircraft Assisted Launch Credit to Stephanie Morris, Jerald.

赴国际水稻所访学情况汇报长江大学农学院邢丹英 2010 年 6 月. 学习目的学习时间、地点学习内容学习收获几点体会汇报提纲.

AAE450 Spring 2009 Brian Erson Attitude Control Systems Trans Lunar Phase Alternative Design Comparison [Brian Erson] [Attitude] 1.

AAE 450 Spring 2008 Steven (“CJ”) Hiu 02/20/2008 Structural Analysis: Overpressure Safety MAT & FAM Coder – Structures CAD – Tanks, Intertank Couplers.

AAE450 Spring 2009 Thermal Transport Subsystems Toy Ball System,100g Payload John Dixon COM GL, Loco PL [John Dixon] [COM GL] 1.

AAE450 Senior Spacecraft Design Dorrie Byford Dorrie Byford Week 7: March 1 st, 2007 Communications Group Leader / Autonomous Rendezvous / Integration.

AAE450 Spring 2009 Lander CATIA Design Communications Group Trans Lunar Phase Group Space Ball Analysis Lander CATIA Design Joshua Elmshaeuser Communications.

AAE 450 Spring 2008 Danielle Yaple 6 March 2008 Avionics Group, GC, CAD, MAT Costs 1.

AAE450 Senior Spacecraft Design Mark Cunningham Mark Cunningham Week 10: March 29 th, 2007 Communications Team Final Presentation Slides – First Draft.

AAE450 Spring 2009 Final Lander Volume and Mass 10kg, 100g, Arbitrary March 12, 2009 Lunar Descent Phase Group [Ryan Nelson] [STRC] 1.

AAE450 Senior Spacecraft Design Goppert, 1 James Goppert Week 8: March 8 th, 2007 Aerodynamics: Reentry Optimization Dynamics and Control: Communication.

PLANETS What is an AU? An astronomical unit (AU) is the average distance of the Earth from the sun. 1 AU = 150 million kilometers.

南水北调东线第一期工程山东段情况简介. 主要汇报内容二、南水北调山东段工程总体布置三、山东段工程项目划分及工程主要建设内容一、南水北调东线工程概况四、前期工作及工程建设进展情况五、工程总投资.

AAE450 Spring 2009 Landing Site Topography Time in Earth and Moon Shadow During Transfer [Kara Akgulian] [Mission Ops] February 11,

24˚South, 134˚ East: 27˚ South, 153˚ East: 43˚ South, 172˚ East:

NH 3rd Stage Trajectory Prediction

Elizabeth Harkness Trajectory Design Group Contact Preliminary Trajectory Model: Vertical Launch AAE 450 Spring 2008.

Space Debris Submitted to the Ilan Ramon Science Olympiad of the Weizmann Institute By the Ramaz Space Rams Ramaz Middle School New York, NY, USA Opening.

continued on next slide

Nicole Bryan 1/31/2008 Avionics Sensor Selection and Link Budget Analysis AAE 450 Spring 2008.

Scale: Kilometers.

continued on next slide

continued on next slide

Three-Body Trajectory Model and Spiral Transfer Matching

Onboard Electrical Equipment

Nicole Bryan Jan. 17th, 2008 Avionics Introductions

Launch Vehicle Selection

Alfred Lynam February 21, 2008 Dynamics and Control D&C simulation code compatibility test with trajectory code. AAE 450 Spring 2008 Dynamics and Control.

Timothy Lorenzana 20 March 2008 Avionics Range Safety / Tracking

Timothy Lorenzana 20 March 2008 Avionics Range Safety / Tracking

[6.2] Reading Graphs.

Launch Vehicle Selection Spring Cannon Launch Vehicle Alternatives

COM 2009 – Opening Reception at Dynamic Earth

Scale: Kilometers.

The Universe and the Solar System

Similarities Differences

continued on next slide

continued on next slide

Presentation transcript:

AAE450 Spring 2009 Ground Stations All Phases and Payloads Trenten Muller March 5, 2009 [Trenten Muller] [COM]

AAE450 Spring 2009 Ground Station List 1.Mt. Pleasant: Hobart, Tasmania AU. 42° S 147° E 2.Irbene, Latvia. 57° N 21° E 3.Rosman, NC USA. 35° N 83° W Top down view of Earth [Trenten Muller] [COM]

AAE450 Spring 2009 Longitude based AltitudesLatitude based worst case scenario altitudes [Trenten Muller] [COM] h km h km h km Hobart km Irbene km Rosman km Price Estimate: Professor Dickey sent us a quote for around $1 million for continuous usage of the Mt. Pleasant Observatory for one year. Because We would not be using more than one station at a time, I believe it is a reasonable assumption that with around $1 million we would be able to rent out as many ground stations as needed for one year, assuming they all charge a similar rate.

AAE450 Spring 2009 Back up Slides [Trenten Muller] [COM]

AAE450 Spring 2009 [Trenten Muller] [COM]

AAE450 Spring 2009 [Trenten Muller] [COM]

AAE450 Spring 2009 [Trenten Muller] [COM]