Skip to content
Engineering your success

Engineering your success

A centre of excellence for aerospace systems, engineering consultancy and space systems development, specialising in entry, descent and landing systems for space vehicles.

  • About Us
    • Our Team
    • Knowledge and Publications
  • What we do
    • Parachutes
    • Entry Systems
    • Inflatable Aerodynamic Decelerators
    • Flexible TPS
    • Testing
    • Aerodynamics
    • Computational Fluid Dynamics
    • More
  • Case Studies
    • ExoMars RSP
    • ExoMars 2016
    • ESA – Development of a Flexible TPS
    • ESA – Huygens Descent Control Sub-System (DCSS)
    • ESA – SuperMax
    • ESA – Earth Return Capsule Dynamic Stability by Balloon Drop Tests
    • ESA – Supersonic Parachute Research
    • NASA – Mars Aerocapture
    • NASA JPL – Mars Science Laboratory Parachute Consultancy
    • More
  • Customers
  • News
  • Careers and Opportunities
  • Contact us
Posted on 12/12/201108/07/2020 by Sarah Griffey

Testing of a two-stage reefed 27m polyconical parachute for the Cirrus Jet

John Underwood and Sam Overend co-authored this article with Cirrus’ Jay Yeakle  Testing of a two-stage reefed 27m polyconical parachute for the Cirrus Jet which was presented at the Aerodynamic Decelerator Systems Technology Conference and Seminar.

Post navigation

Next PostNext Hypercone inflatable supersonic decelerator

ENGINEERING YOUR SUCCESS

Search

Recent Posts

  • ESA Ministerial to discuss next steps for ExoMars
  • Suspension of the ExoMars Programme
  • ExoMars Dynamics Extraction Test Campaign Concluded
  • ExoMars to take off for the Red Planet in 2022
  • European Space Agency Mars parachute tests
Proudly powered by WordPress