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Showing 1 to 3 of 3 for “"Aerospike Nozzle"”.

  1. Design and Analysis of a Reusable N2O-Cooled Aerospike Nozzle for Labscale Hybrid Rocket Motor Testing

    <p>A reusable oxidizer-cooled annular aerospike nozzle was designed for testing on a labscale PMMA-N<sub>2</sub>0<a href="http://digitalcommons.calpoly.edu/cgi/ir_submit.cgi#_ftn1">[1]</a> hybrid rocket motor at Cal Poly-SLO.<a …

    calpoly Repository record for Design and Analysis of a Reusable N2O-Cooled Aerospike Nozzle for Labscale Hybrid Rocket Motor Testing (opens in a new tab)

  2. Hole-Type Aerospike Compound Nozzle Thrust Vectoring

    Compound aerospike nozzles were designed and tested as part of an ongoing experimental study to determine the feasibility of thrust vectoring an aerospike nozzle with the addition of a secondary port. Earlier phases of the study have indicated that a compound aerospike nozzle could provide …

    calpoly Repository record for Hole-Type Aerospike Compound Nozzle Thrust Vectoring (opens in a new tab)

  3. Aerospike Rocket Motor Structural Webbing

    … of technologies relating to the annular aerospike nozzle. In order to prevent undesirable deflection of the cantilevered spike, a structural stiffening web, referred to as “The Spider,” is proposed. The Spider resembles a three-spoked wheel, with the aerospike held by the inner hub and …

    calpoly Repository record for Aerospike Rocket Motor Structural Webbing (opens in a new tab)