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Design of a fast responding start-up mechanism for bi-propellant fueled engine for miniature UAV applications

Jonas Galle (UGent) and Sebastian Verhelst (UGent)
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Keywords
liquid fueled, H2O2, UAV, rocket engine

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Citation

Please use this url to cite or link to this publication:

Chicago
Galle, Jonas, and Sebastian Verhelst. 2013. “Design of a Fast Responding Start-up Mechanism for Bi-propellant Fueled Engine for Miniature UAV Applications.” In SAE Technical Paper Series.
APA
Galle, Jonas, & Verhelst, S. (2013). Design of a fast responding start-up mechanism for bi-propellant fueled engine for miniature UAV applications. SAE technical paper series. Presented at the AeroTech Congress & Exhibition (SAE - 2013).
Vancouver
1.
Galle J, Verhelst S. Design of a fast responding start-up mechanism for bi-propellant fueled engine for miniature UAV applications. SAE technical paper series. 2013.
MLA
Galle, Jonas, and Sebastian Verhelst. “Design of a Fast Responding Start-up Mechanism for Bi-propellant Fueled Engine for Miniature UAV Applications.” SAE Technical Paper Series. 2013. Print.
@inproceedings{4116976,
  articleno    = {2013-01-2305},
  author       = {Galle, Jonas and Verhelst, Sebastian},
  booktitle    = {SAE technical paper series},
  issn         = {0148-7191},
  keyword      = {liquid fueled,H2O2,UAV,rocket engine},
  language     = {eng},
  location     = {Montreal, Canada},
  pages        = {9},
  title        = {Design of a fast responding start-up mechanism for bi-propellant fueled engine for miniature UAV applications},
  url          = {http://dx.doi.org/10.4271/2013-01-2305},
  year         = {2013},
}

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