1 / 5

Elizabeth Harkness Trajectory Design Group Contact Preliminary Trajectory Model: Vertical Launch

Elizabeth Harkness Trajectory Design Group Contact Preliminary Trajectory Model: Vertical Launch. Comparison of Launch System Performance. Comparison of altitudes using vertical launch trajectory. -Plot generated by: Elizabeth Harkness -From code generated by: Junichi Kanehara and

taffy
Download Presentation

Elizabeth Harkness Trajectory Design Group Contact Preliminary Trajectory Model: Vertical Launch

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. Elizabeth HarknessTrajectory Design Group ContactPreliminary Trajectory Model:Vertical Launch AAE 450 Spring 2008

  2. Comparison of Launch System Performance Comparison of altitudes using vertical launch trajectory. -Plot generated by: Elizabeth Harkness -From code generated by: Junichi Kanehara and Amanda Briden -with assistance from: Elizabeth Harkness AAE 450 Spring 2008 Trajectory Optimization

  3. Comparison of Launch System Performance 1. Initial conditions for Balloon and Aircraft Launches found in cited articles. AAE 450 Spring 2008 Trajectory Optimization

  4. Model Assumptions • Values input into code are from Vanguard data Table 20. Payload of 100 lbs, orbit at 180 statute miles. • All stages are modelled vertically. • Poor assumption • Does not take into account the lengthy portion of trajectory through the atmosphere. • Preliminary test of trajectory code and comparison of three of the launch methods AAE 450 Spring 2008

  5. References Heister, S., “AAE 539 atmosphere4” [https://engineering.purdue.edu/AAE/Academics/Courses/aae539/2008/std.%20atmosphere%20matlab%20code%20for%20HW1%20Prob2.] Howell, K., “AAE 340 Dynamics and Vibrations," Numerical Integration and Spherical Coordinates, Purdue University, West Lafayette, IN, 2006. Klauans, B., and Raughards, J., “The Vanguard Satellite Launching Vehicle An Engineering Summary," The Martin Company, Engineering Report No. 11022, Baltimore, MD, April 1960. (pp.170) Kloster, K., and Longuski, J., Personal Conversation, January 15-16, 2008. Longuski, J., “AAE 508 Optimization in Aerospace Engineering Lectures," Lecture #10, Purdue University, West Lafayette, IN, 2008, pp. 62. Wade, M., “Cape Canaveral," Encyclopedia Astronautica.  [http://www.astronautix.com/sites/capveral.htm.  Accessed 1/16/08.] AAE 450 Spring 2008 Trajectory Optimization

More Related