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

Slides:



Advertisements
Similar presentations
Chapter 7: Work (Ewen et al. 2005) Objectives: Define power and solve power problems Define power and solve power problems.
Advertisements

Lunar Lander Power Systems
Today’s Kaupapa: 1) Calculate the position of the centre of mass 2) Describe the motion of an object in terms of its centre of mass 3) Analyse 2D collisions.
AAE450 Spring 2009 UHF Lander-Rover COM Systems Toy Ball Shell Structure Communications Group Trans Lunar Phase Group Toy Ball Analysis Lander CATIA Design.
AAE450 Spring 2009 Final Presentation Draft Slides Description: Some draft slides and ideas 3/26/09 Kris Ezra Attitude 1.
AAE450 Spring 2009 Time to Complete 50m/s ΔV & 100g Payload System Overview Brittany Waletzko 100g Payload Integration Manager Translunar/OTV Phase Week.
AAE450 Spring 2009 Hopper Trajectory February 26, 2009 [Alex Whiteman] [Mission Ops] [Lunar Descent] Page 1.
AAE450 Spring 2009 Attitude Determination in Low Earth Orbit Description: Research Attitude Determination Systems Filter Pertinent Reference Material from.
AAE450 Spring 2009 Slide 1 of 7 Orbital Transfer Vehicle (OTV) Thermal Control Ian Meginnis February 26, 2009 Group Leader - Power Systems Phase Leader.
AAE450 Spring 2009 Kelly Leffel 3/26/09 Structures and Thermal Lunar Descent Phase Lander Integration Lander Thermal Control (Day) Kelly Leffel Structures.
AAE450 Spring 2009 Ground Stations All Phases and Payloads Trenten Muller March 5, 2009 [Trenten Muller] [COM]
AAE450 Spring 2009 Locomotion Phase: Propulsion System X1 February 5, 2009 Ryan Lehto Propulsion Locomotion CAD Designer.
AAE450 Spring 2009 Week 4 Presentations [Solomon Westerman][PM]
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 Lunar Descent Final Numbers Josh Lukasak Attitude Group Lead Lunar Decent Phase Lead 03/12/09 [Josh Lukasak] [Attitude] (1)
AAE450 Spring 2009 Link Budget Michael Christopher -Communications Group -TLI Phase Group 1 OF 3Michael Christopher - COM.
AAE450 Spring 2009 Locomotion Alternatives Thursday February 19, 2009 Ryan Lehto Propulsion Group, Locomotion Phase, CAD Designer.
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 Electronic Hardware Systems Communications Trans-Lunar Phase Joshua Elmshaeuser Communications 1.
AAE450 Spring 2009 Hopper Design Alternative Josh Lukasak Attitude Group Lead Lunar Decent Phase Lead 02/26/09 [Josh Lukasak] [Attitude] (1)
AAE450 Spring Lunar Descent Attitude Control Analysis Christine Troy Assistant Project Manager Webmaster Lunar Descent Attitude Control Analysis.
AAE450 Spring 2009 X 0 Power System Solar - Battery Solar arrays Tony Cofer- Power System.
AAE450 Spring 2009 Week 4 Project Timeline [Solomon Westerman] [PM]
AAE450 Spring Gram Lander CATIA Design Communications Group Trans Lunar Phase Group Toy Ball Analysis Lander CATIA Design Joshua Elmshaeuser Communications.
AAE450 Senior Spacecraft Design 2/15/2007 Scott 1 Ryan Scott Week 5: February 15th, 2007 Power Group Leader TC, TV, dE, aM, dM, aM, CS1, CS2, CS3 *WITH.
AAE 450 Spring 2008 Justin M. Rhodes Avionics – Telecommunications Webmaster Telecommunications and Wiring.
Phase Difference = Phase Difference = 0.05.
A spring with a mass of 6 kg has damping constant 33 and spring constant 234. Find the damping constant that would produce critical damping
AAE 450 Spring 2008 Nicole Bryan Avionics Final Presentation Slides 1.
AAE450 Spring 2009 OTV 3-D GEOMETRY & INTEGRATION Korey LeMond STRC/THM/INTEG/CAD GL, Locomotion Phase OTV Phase [Korey LeMond] [STRC/THM/INTEG/CAD GL,
AAE450 Spring 2009 Kelly Leffel 3/0509 Structures and Thermal Lunar Descent Phase Lander Integration Lander Thermal Control Kelly Leffel Structures and.
AAE450 Spring 2009 BAE Single Board Computer Ground Based Systems Communications Group Trans Lunar Phase Group Joshua Elmshaeuser Communications 1.
1 AAE 450 Spring 2008 David Childers February 7, 2008 Interface Structures (skirts) Center of Mass Code Structures Cost Code.
AAE450 Spring 2009 Launch Vehicles Zarinah Blockton Mission Operations 1/29/2009 Blockton Ops.
AAE450 Spring 2009 Thermal Transport Internal Heat Sources External Insulation COM GL Locomotion Phase Lead [John Dixon] [COM] 1.
1 How to design or select an antenna? Communications Crosslink scientific/housekeeping data (emitter & receiver sat) G/S link scientific data (emitter.
AAE450 Spring 2009 Communications Ground Stations Communication Equipment Alternative Landing Method March 26, 2009 [Trent Muller] [COM]
AAE450 Spring 2009 Rover Power Toy Ball Power (Budget and Resizing) Jeff Knowlton [Jeff Knowlton] [Power] 1.
Formative Assessment. 1. If a heater is 78.0% efficient, how much fuel energy would it consume to provide 120. J of useful heat? How much useful heat.
Model No. CK1000MN / CK1000MNAL Automatic Lift is Optional Organic Food Waste Composter 1200 KG Processing Capacity.
AAE 450 Spring 2008 Jesii Doyle 1/17/2008 Internal Structure, Mounting Materials Initial Mounting Materials Research.
Force of Gravity Pre-Lab Are the forces of gravity acting on the two students different? What is another term that means the force of gravity? Weight –
Formative Assessment. 1. A 130. gram uniform meter stick has a 22.0 g clamp on the 23.0 cm mark, where would you clamp a 35.0 g clamp to make the meter.
AAE450 Spring 2009 Lunar Lander Power Systems Thursday March 12 th Adham Fakhry Power Group Lunar Lander Descent Night Thermal.
AAE450 Spring 2009 Brian Erson Attitude Control Systems Trans Lunar Phase Alternative Design Comparison [Brian Erson] [Attitude] 1.
A. Bertarelli CERN TS – MME Group 1 CERN European Organization for Nuclear Research Actuating system of the LHC Collimators (Phase 1) Main Features.
AAE450 Spring g Locomotion Thursday March 5, 2009 Ryan Lehto Propulsion Group, Locomotion Phase, CAD Designer.
AAE450 Spring 2009 Thermal Transport Subsystems Toy Ball System,100g Payload John Dixon COM GL, Loco PL [John Dixon] [COM GL] 1.
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 Spring 2009 Kelly Leffel 2/5/09 Structures and Thermal Lunar Descent Phase Kelly Leffel Structures and Thermal 1.
A&AE 450 – Senior Design Un-pressurized Surface Vehicles, Local Science Issues and Robotic Exploration February 13, 2000 Christopher Burnside.
AAE450 Spring 2009 Lunar Night and Lander Power System Adham Fakhry February 26th, 2009 Power Group Lunar Descent Phase Passive Thermal Control for Lunar.
AAE450 Senior Spacecraft Design Mark Cunningham Week 6: February 22 nd, 2007 Communications Team, Comm. SATs CAD, TV/ET/MT Groups Communication Satellites.
The HOPPER: Engineering Analysis Update Team Meathead March 9, 2005.
AAE450 Spring 2009 Kelly Leffel Structures and Thermal [Kelly Leffel] [Structures and Thermal]
AAE450 Spring 2009 Power Systems for Lander Adham Fakhry [Adham Fakhry] [Power]
Power Screws. Ball Screws Problem A stepper motor rotating at 120 rpm is directly coupled to a power screw with a pitch of 1 mm. 1.How fast can the.
AAE450 Spring 2009 Attitude Determination in Low Earth Orbit Description: Determine Attitude Accuracy Upper and Lower Bound Recommend Addition of Sun Sensor.
Nicole Bryan 1/31/2008 Avionics Sensor Selection and Linkbudget Analysis AAE 450 Spring 2008.
Rover Communication Subsystems
Motorized Antenna Mount
Rover/Lander Power Budgets
Nicole Bryan Avionics Final Presentation Slides
Onboard Electrical Equipment
Final Presentation Slides
100 g Locomotion Thursday March 26, Ryan Lehto Propulsion Group
IT 318: M5 Motors: Questions IT M6.
FOUR-WHEEL STEERING SYSTEM
Sarah Shoemaker 3/20/2008 Structures, Gondola Design, Tanks, CAD Final Slides AAE 450 Spring 2008 Structures.
Presentation transcript:

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

AAE450 Spring OF 5Michael Christopher - COM Antenna MountBase Plate Stepper Gear Motor

AAE450 Spring OF 5Michael Christopher - COM  Mass: 2*( kg/motor) + 0.1kg = kg  Power Consumption: Watts  Cost: 2*($16.75 /motor) + ~$50 Al = $83.50

AAE450 Spring OF 5Michael Christopher - COM

AAE450 Spring OF 5Michael Christopher - COM Prices from McMaster-Carr