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Showing 1 to 7 of 7 for “"Aerospike"”.

  1. 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)

  2. Aerospike Thrust Vectoring Slot-Type Compound Nozzle

    A study of thrust vectoring techniques of annular aerospike nozzles was conducted. Cold-flow blow-down testing along with solid modeling and rapid prototyping technology were used to investigate the effects of slot size, placement, geometry and orientation. The use of slot-type compound nozzles …

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

  3. 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)

  4. 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)

  5. Wake closure conditions in plug nozzle flowfields

    The aerospike, of plug, nozzle is being proposed for future space launch vehicle applications. The design of the nozzle involves complex wake structures that directly affect engine performance. In particular, the closed or open wake condition of the flow determines the dependence of the base …

    washington Repository record for Wake closure conditions in plug nozzle flowfields (opens in a new tab)

  6. Improving the Performance of Re-entry Vehicle in Hypersonic Flow by Morphing Nose cone by Bio-Mimicking Honey Bee Abdomen

    … nosecone morphing honey bee abdomen with flat D-aerospike. The presence of a strong bow shock in honey bee abdomen morphed nosecone without spike generates significant drag, which diminishes in its alternate position. During the honey bee 's extension, both at 2.5 degrees and 5 degrees, the drag …

    southwales Repository record for Improving the Performance of Re-entry Vehicle in Hypersonic Flow by Morphing Nose cone by Bio-Mimicking Honey Bee Abdomen (opens in a new tab)

  7. Fluidic Thrust Vectoring of Actively Controlled Nozzle Flows

    L'abstract è presente nell'allegato / the abstract is in the attachment

    poli-torino Repository record for Fluidic Thrust Vectoring of Actively Controlled Nozzle Flows (opens in a new tab)