1 / 4

Tim Lorenzana 1/16/2008 Avionics Recovery/Termination

Tim Lorenzana 1/16/2008 Avionics Recovery/Termination. Rocket Recovery. Parachute Impact System Airbags Retro Rockets Rotating Wing Helicopter Action. Nylon 496.05grams/meter $12.14meter Launch Vehicle Mass 100.5kg Parachute Diameter 1.06meters Parachute Mass 2.22kg

Olivia
Télécharger la présentation

Tim Lorenzana 1/16/2008 Avionics Recovery/Termination

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. Tim Lorenzana1/16/2008AvionicsRecovery/Termination AAE 450 Spring 2008

  2. Rocket Recovery • Parachute • Impact System • Airbags • Retro Rockets • Rotating Wing • Helicopter Action Nylon 496.05grams/meter $12.14meter Launch Vehicle Mass 100.5kg Parachute Diameter 1.06meters Parachute Mass 2.22kg Parachute Cost $54.27 AAE 450 Spring 2008 Avionics

  3. Rocket Termination • Federal Aviation Regulations Require Our Launch Vehicle Have the Capability to Self Destruct Before Causing Damage or Harm to People or Property. Future Work • Further Analysis of Recovery Options • Greater Understanding of Termination Requirements and Guidelines AAE 450 Spring 2008 Avionics

  4. Basic Parachute Calculations Drag Force Weight At Full Chute Deployment; Descent Velocity Chute Diameter AAE 450 Spring 2008 Avionics

More Related