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- Domain created: 2001-10-02T15:14:21Z
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- Location: United States
- Latitude: 37.751
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Websites Listing
We found Websites Listing below when search with nakka-rocketry.net on Search Engine
Richard Nakka's Experimental Rocketry Site
Web Solid Rocket Motor Design SRM is an MS EXCEL spreadsheet that takes user-inputted motor and grain geometry data and computes Kn over the duration of the motor burn, …
Nakka-rocketry.netRichard Nakka's Experimental Rocketry Site
Web What exactly does this mean? In hindsight, the reason that I did not have success with the zinc/sulfur or blackpowder propellants was certainly due to the methodology I employed …
Nakka-rocketry.netRichard Nakka's Experimental Rocketry Site
Web Figure 1 shows a stable rocket, with the CP aft of the CG. In this figure, the rocket is illustrated in a simplified form. This is because this principle is true for a body of any shape, not only for a finned rocket (for example, …
Nakka-rocketry.netRichard Nakka's Experimental Rocketry Site
Web This webpage provides an introduction to rocketry and how model rocketry can serve as a basis for learning about science and engineering. Includes links to several resources for learning how to build model rockets as well …
Nakka-rocketry.netRichard Nakka's Experimental Rocketry Site
Web This web page describes the "classic" sugar-based rocket propellant comprised of a fused mixture of Potassium Nitrate serving as the oxidizer, and Sucrose (table sugar) serving as the fuel and binder. This propellant …
Nakka-rocketry.netRichard Nakka's Experimental Rocketry Site
Web In this series of web pages, my goal is to "distill and compile" my knowledge gained over the years, fortified by my rocketry exeriences, into a guide for likewise passionate …
Nakka-rocketry.netRichard Nakka's Experimental Rocketry Site
Web Aug 26, 2001 · The Cirrus One rocket was equipped with a set of three aluminum alloy (6061-T6) fins, of 0.063 inch (1.6 mm) thickness. The fin attachment method was radically different than the method used for the …
Nakka-rocketry.netRichard Nakka's Experimental Rocketry Web Site
Web Richard Nakka's Experimental Rocketry Web Site Effects of Heating Sorbitol Effects of Overheating I first became aware of the Potassium Nitrate/Sorbitol (KNSB) rocket propellant in 1996, when I learned that it …
Nakka-rocketry.netRichard Nakka's Experimental Rocketry Site
Web This web page presents details regarding the design of a strain gage based load cell that can be used, in conjunction with an electronic data acquisition (DAQ) system, for static thrust measurement of a rocket motor.
Nakka-rocketry.netRichard Nakka's Experimental Rocketry Site
Web Basic Dimensions and Configuration. The Impulser motors have an outside diameter of 1.50 inches (38mm). Impulser has an overall length of 13.6 inches (345mm), Impulser-X has …
Nakka-rocketry.netRichard Nakka's Experimental Rocketry Web Site
Web For KNPSB, the casting temperature is in the range of 110 o-115 o C (230 o-240 o F.). This is a lower casting temperature than KNSB. The KNPSB powder begins to melt at 70 o C. …
Nakka-rocketry.netRichard Nakka's Experimental Rocketry Site
Web Nozzle The nozzle is a conical profiled, deLaval supersonic type machined from low-carbon steel (AISI 1018). The 30 o convergent and 12 o divergent half-angles are the same as …
Nakka-rocketry.netRichard Nakka's Experimental Rocketry Site
Web This igniter design is based on a concept pioneered by rocketry experimenter Rob Furtak, who has used the Mini-bulb igniter with great success in his rocketry work. The igniter …
Nakka-rocketry.netRichard Nakka's Experimental Rocketry Site
Web Do your utmost to keep Amateur Experimental Rocketry safe, not only for your own sake, but also for the sake of all participants of this challenging, educational and uniquely "out …
Nakka-rocketry.netRichard Nakka's Experimental Rocketry Web Site
Web Taking equations 3, 4, 7 & 9, it is possible to express the area ratio, A/A*, in terms of. the Mach number of the flow. The area ratio is simply the cross-sectional area at any point …
Ia601808.us.archive.orgRichard Nakka's Web Site - Archive.org
Web 2/6/2020 Richard Nakka's Experimental Rocketry Site www.nakka-rocketry.net/thermites.html 7/ 8 C on c l u s i on s These experiments demonstrated that …
Archive.orgExperimental Rocketry Web Site - Internet Archive
Web 2/6/2020 Richard Nakka's Experimental Rocketry Site www.nakka-rocketry.net/igniter.html 4/ 13 C h am b e r P re s s u re d u e t o I gn i t e r C om b u s t i on
Ia601808.us.archive.org
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