We think you have liked this presentation. If you wish to download it, please recommend it to your friends in any social system. Share buttons are a little bit lower. Thank you!
Presentation is loading. Please wait.
Modified over 4 years ago
AAE450 Spring 2009 Cost Analysis, Redux Solomon Westerman Week9: 3/12/09 [Solomon Westerman][PM]Page 1/3
AAE450 Spring 2009 [Solomon Westerman][PM] Page 2/3 Total Cost ($M USD) Launch4.4 R&D2.3 Integration4.9 Purchase7.2 Overhead8.0 Total26.9 GLXP Prize ($M USD) Grand Prize20.0 Lunar Night1.0 Total21.0 Lose $5.9 M in 2012 USD!
AAE450 Spring 2009 $/kg Dry Lander on Surface 100g$295,000 10kg$257,000 Arbitrary$126,000 [Solomon Westerman][PM] Page 3/3 $/kg Payload to Lunar Base First Launch$170,000 Marginal Cost$168,000
AAE450 Spring 2009 Backup Slides [Solomon Westerman][PM]
AAE450 Spring 2009 Costing Model Differences 1.Overhead –100g, 10kg 15 engineers @ 3 years @ 150k each 3 STK license, 15 MATLAB license –Arbitrary 100 engineers @ 3 years @ 150k each 10 STK license, 75 MATLAB license 2.R&D –100g, 10kg 20 Engineers @ 150k salary each + 50k per month equipment increases reliability by 2% per month –Arbitrary 40 Engineers @ 150k salary each + 50k per month equipment increases reliability by 2% per month 3.Integration –100g, 10kg $10k / kilogram –Arbitrary $10k / kilogram [Solomon Westerman][PM]
AAE450 Spring 2009 Reliability Analysis Solomon Westerman, PM Week 5, 2/12/09 [Solomon Westerman] [PM] 1.
Lunar Lander Power Systems
AAE450 Spring 2009 Brian Erson Attitude Control Systems Trans Lunar Phase [Brian Erson] [Attitude] 1.
AAE450 Spring 2009 Propellant Choice and Mass Estimates for the Translunar OTV Week 2 Presentation Thursday, Jan 22, 2009 Brad Appel Propulsion Group.
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 Lunar Lander Main Engine 1.Overall system design 2.Performance Optimization 3.Jointly worked on thrust and CEA based script to allow.
AAE450 Spring 2009 Power Group Tony Cofer Surviving the Lunar Night 03/25/09 [Tony Cofer] [Power] Page 1.
The Lander is at a 25 km Lunar altitude and an orbital period of approximately 110 minutes. After separation occurs the Lander is completely self sufficient.
AAE450 Spring 2009 Lunar Lander Propulsion System 100g, 10kg and Large Payload cases Thaddaeus Halsmer Thursday, April 9, Lunar Lander propulsion.
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 Kelly Leffel 3/26/09 Structures and Thermal Lunar Descent Phase Lander Integration Lander Thermal Control (Day) Kelly Leffel Structures.
AAE450 Spring 2009 Brian Erson Attitude Control Systems Trans Lunar Phase Alternative Design Analysis Cold Xe Gas Thrusters [Brian Erson] [Attitude] 1.
AAE450 Spring 2009 Lander Phase: Hybrid Propulsion System Propulsion System Sizing and Inert Mass Analysis Hopper and Rover Designs for 10kg Payload Hopper.
AAE450 Spring 2009 Week 9 [Solomon Westerman] [PM] Design Freeze on Thursday night!
AAE450 Spring 2009 Analysis of Trans-Lunar Spiral Trajectory [Levi Brown] [Mission Ops] February 12,
AAE450 Spring Attitude Control – Arbitrary Payload Christine Troy Assistant Project Manager Webmaster Lunar Descent Attitude Control Analysis Design.
AAE450 Spring Spinning Descent and Compressed Gas Hopper Christine Troy Assistant Project Manager Webmaster Lunar Descent Attitude Control Analysis.
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]
© 2020 SlidePlayer.com Inc. All rights reserved.