• DocumentCode
    711413
  • Title

    LDSD supersonic Flight Dynamics Test 1: Post-flight reconstruction

  • Author

    Blood, Eric ; Ivanov, Mark ; O´Farrell, Clara ; Ginn, Jason ; Kutty, Prasad ; Karlgaard, Chris ; Dutta, Soumyo

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • fYear
    2015
  • fDate
    7-14 March 2015
  • Firstpage
    1
  • Lastpage
    15
  • Abstract
    The Low Density Supersonic Decelerator project´s first Supersonic Flight Dynamics Test (SFDT) occurred on June 28, 2014, off the west coast of Kauai, Hawaii, over the Pacific Ocean. The test vehicle traveled to speeds above Mach 4 and to an altitude of over 200,000 feet. This flight, although classified as a test architecture shake-out flight, tested two technologies: a robotic class Supersonic Inflatable Aerodynamic Decelerator and a Supersonic Disksail Parachute. The reconstruction team was tasked with collecting all relevant pre-flight and flight data to accurately reconstruct the trajectory and technology performance during the science phase of the flight. Furthermore, the reconstruction team has been involved with reconstructing and exploring all aerodynamic and test vehicle properties that affected the entire flight phase. This reconstruction provided insight into the technology performance, which is a key deliverable for the LDSD project, as well as provided insight into lessons learned for subsequent SFDT flights, in the fields of data recovery, reconstruction, and pre-flight trajectory simulations.
  • Keywords
    aerodynamics; aerospace simulation; aircraft testing; supersonic flow; LDSD project; LDSD supersonic flight dynamics test; Mach 4; SFDT flights; data recovery; flight data; low density supersonic decelerator project; post-flight reconstruction; pre-flight trajectory simulations; robotic class supersonic inflatable aerodynamic decelerator; supersonic disksail parachute; test architecture shake-out flight; test vehicle properties; Accuracy; Global Positioning System; Instruments; Robustness; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2015 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    978-1-4799-5379-0
  • Type

    conf

  • DOI
    10.1109/AERO.2015.7119246
  • Filename
    7119246