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Experimental Studies of Protrusion-Inserted Hybrid Rocket Motor with Varying L/D Ratio
- Source :
- Journal of Spacecraft and Rockets. 58:134-147
- Publication Year :
- 2021
- Publisher :
- American Institute of Aeronautics and Astronautics (AIAA), 2021.
-
Abstract
- This study investigates the effects of single, double, and multi-protrusion on the performance of a hybrid rocket with two different L/D ratio motors, mainly 12.5 and 18. Wax and gaseous oxygen wer...
- Subjects :
- 020301 aerospace & aeronautics
Wax
Materials science
business.product_category
integumentary system
Gaseous oxygen
Aerospace Engineering
02 engineering and technology
Characteristic velocity
Boundary layer thickness
Rocket motor
01 natural sciences
010305 fluids & plasmas
0203 mechanical engineering
Rocket
Space and Planetary Science
visual_art
0103 physical sciences
Heat transfer
visual_art.visual_art_medium
Composite material
business
Subjects
Details
- ISSN :
- 15336794 and 00224650
- Volume :
- 58
- Database :
- OpenAIRE
- Journal :
- Journal of Spacecraft and Rockets
- Accession number :
- edsair.doi...........96eaae9a36c6eb4981b4d7a823d85eec
- Full Text :
- https://doi.org/10.2514/1.a34759