Overview of a 4-inch OD Paraffin-Based Hybrid Sounding Rocket Program
Author:
Affiliation:
1. Lockheed Martin
2. Sr. Research Engineer, Dept of Aeronautics and Astronautics, Stanford University, Member AIAA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-3822
Reference11 articles.
1. Development and testing of paraffin-based hybrid rocket fuels
2. Flight Demonstration of the High Burning Rate Hydrocarbon-Based Hybrid Rocket Fuels
3. Overview of Hybrid Sounding Rocket Program
4. 346in 11859m 11560m 11045m 10546m 10191m Table I:FuelPort Diameter andOxInjector AreaCombinations Figure3: Cross-Sectionof ParaffinFuel Grain
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