

What is this Web Site all about?My goal in producing this web site is to share experiences, ideas and technical details of Amateur Experimental Rocketry with others around the world who have a similar interest. It is also my dream to help inspire a future generation of engineers and scientists who will some day take us to Mars and beyond... Between the years 1972, when I launched my first amateur rocket, and 1986, I built and flew many rockets, powered by motors which I had developed. During this time, I kept detailed notes of all my work, carefully logged all the flights and other tests, and took countless photographs. In this web site, I am presenting at least a portion of this work. As well, I am presenting more contemporary ideas and activities, which followed the reemergence of my rocketry work in 1997, after a decade on the "back burner". In addition to my own work, I am including some remarkable work done by others in this exciting field! Amateur Experimental Rocketry ?Amateur Experimental Rocketry is, in my humble opinion, one of the most challenging, educational and exciting hobbies! Unlike Model Rocketry or High Power Rocketry, experimental rocketry is an activity whereby rockets are designed and constructed entirely from "scratch" -- including motor and propellant. No significant components are commercially manufactured. The goal of Amateur Experimental Rocketry (AER), often simply referred to as Amateur Rocketry or Experimental Rocketry, is to design, build, test and launch rockets. In this context, rocket may refer to the motor itself, or to a complete vehicle that consists of motor, fuselage (and stabilizing devices such as fins), nosecone, and payload. One of the greatest challenges is to develop and build such a motor, one that is safe to produce and operate, reliable, and one that provides predictable and consistent performance. A second big challenge is to develop a recovery system, such as parachute deployment, that operates with a high degree of reliability under the demanding conditions of launch followed by high speed or high altitude flight. Striving to achieve these goals (and many others) and to overcome the inevitable obstacles, is what makes this such a challenging (and at times frustrating) and educational pastime, and one that requires diversified skills combined with a good dose of ingenuity. The outcome of all this, more often than not, is that one learns to genuinely comprehend that which is colloquially known as Rocket Science. It might be said, then, that Model Rocketry and High Power Rocketry are best suited to those who wish to make and fly rockets, and Experimental Rocketry is perhaps best suited to those who rather wish to make rockets fly. Contents of this web site are presented for informational purposes only. Author of this web site cannot assume responsibility for the use readers make of the information presented herein or the devices resulting therefrom. Amateur Experimental Rocketry has many inherent hazards that must be fully understood before one can consider becoming actively involved. Safety must always be considered as top priority. Anything less is a disservice to all Amateur Experimental Rocketry enthusiasts. If you do not have first-rate common sense, or if you are willing to take shortcuts that compromise safety, then AER is not for you. Latest news
Please take note of my e-mail address:
Oct. 19, 2003 --I've added design charts (Kn vs. Pressure) for the RNX propellants in the Performance Data page. I plan to wrap up the RNX pages in the near future, as I have finally completed the characterization work (was more of a challenge than I'd anticipated!). In other news, I'm currently building a new rocket that I plan to launch in November (haven't come up with a name for it yet...!)
Aug. 23, 2003 --The webpage on Igniters has been updated with details on the "Ferocious" igniter that was developed for use with the RNX composite propellants.
June 12, 2003 --The webpage on RNX composite propellants was started some time ago, and
is currently under construction. I plan to regularly work on completing
this page over the next few months. Concurrently, I am in the process of
"characterizing" the RNX propellants, which involves experimentally
determining such key design parameters as burn rate with respect to
chamber pressure, C-star, specific impulse, heat of combustion, etc.
Although this has been going quite well, there have been a few "glitches" that have made the process somewhat more challenging than originally
anticipated. (e.g. see "Sneak Preview" page). Such is AER ...!
Coming in the months ahead...
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General
- Safety (external link)
- Photo Galleries
Jul. 15/00
- Rocket Video Clips
- Who is Richard Nakka?
- Rocketry related Technical References
Nov.1/03
- Rocketry software
Dec.21/02
- Links to Other Interesting Websites
Nov. 2/03
- Activities of other AER enthusiasts
Mar. 3/00
- Sneak Preview
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Nov. 2/03
Motors
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- B-200 Rocket Motor ("H" Class)
Mar.25/02
- C-400 Rocket Motor ("I" Class)
Oct.23/99
- A-100 Rocket Motor ("G" Class)
Oct.23/99
- Kappa Rocket Motor ("K" class)
Apr.13/01
- Juno Rocket Motor ("J" class) -- Preliminary Design
Nov.25/01
- Lambda Rocket Motor ("L" class) -- Preliminary Design
- Juno Rocket Motor -- Static Test JDX-001 Report
- Lambda Rocket Motor -- Static Test LDX-001 Report
- PVC Rocket Motors -- Introduction and Performance ("G", "H", & "I" motors)
- PVC Rocket Motors -- Design
- PVC Rocket Motors --Tools
- PVC Rocket Motors --Construction
- PVC Rocket Motors -- Igniters, Mounts & Conclusion
June 16/02
- PVC Rocket Motors -- Introduction & Performance ("J/K" Class motors)
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- PVC Rocket Motors - Tools,Construction & Conclusion ("J/K" Class motors)
February 8/03
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- K1000 PVC Rocket Motor
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- Kappa ("K" class) rocket motor -- preliminary design
Jan.2/00
- Kappa-DX rocket motor -- Static Test KDX-001 Report
- Kappa-DX rocket motor -- Static Test KDX-002 Report
- Kappa-SB rocket motor -- Static Test KSB-001 Report
Oct.10/00
- Kappa-SB rocket motor -- Static Test KSB-002 Report
- Epoch rocket motor ("I" Class composite)
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- Paradigm rocket motor ("J" Class composite)
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- Calculation of Total and Specific Impulse from Test Data
May 17/01
- Igniter Systems
Aug. 23/03
- Case-bonding of a High-Modulus Propellant Grain
- Thermal Protection for Rocket Motor Casings
- Rocket Motor Design Charts -- Chamber Pressure
Propellants
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- Amateur Experimental Solid Propellants
- The Potassium Nitrate/Sucrose Propellant (KNSU)
April 15/03
- The Potassium Nitrate/Dextrose Propellant (KNDX)
June 1/02
- The Potassium Nitrate/Sorbitol Propellant (KNSB)
June 16/02
- KNSU Propellant Chemistry and Performance Characteristics
Nov. 13/99
- KNDX Propellant Chemistry and Performance Characteristics
Dec. 10/00
- KNSB Propellant Chemistry and Performance Characteristics
Nov. 13/99
- The Potassium Nitrate/Epoxy Composite Propellant (RNX)
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Oct.19/03
- INERT Propellant
- Propellant Burn Rate
June 21/03
- Burn Rate Determination from a Pressure-time Trace
- Strand Burner for Burn Rate Measurements
- KN-Dextrose & KN-Sorbitol Propellants -- Burn Rate Experimentation
July 1/02
- Effect of Potassium Nitrate Grade on Propellant Performance
Sept. 15/01
- The KN-Sucrose Propellant -- A Historical Look Back
Nov. 25/01
- Problems relating to the casting of sleeve-bonded propellant segments
for the Kappa-DX rocket motor Static Test KDX-001- Propellant Igniteability Experiment
- Propellant Inhibitor Experiment
- Experiments with Potassium Nitrate - Epoxy Formulations
- Burn Characteristics of Sorbitol Based Propellants
Testing
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- Rocket Motor Static Testing
Aug. 5/00
- STS-5000 Static Test Stand
- Hydraulic Load Cell for Thrust measurement
July 13/03
- Strain Gage Load Cell for Thrust measurement
Rockets
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- Boreas 1 Rocket
- Launch Report -- Epoch Rocket Motor (unofficial) Inaugural Flight
- Launch Report - Boreas 1 Inaugural Flight
- Launch Report - Boreas 1, Flight #2
- Launch Report - Boreas 1, Flight #3
- Launch Report - Boreas 1, Flight #4
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- Launch Report - Boreas 1, Flight #5
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- Launch Report - Frostfire One
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- Cirrus Project
Feb.7/02
- Cirrus One Launch Report
Mar. 20/03
- Cirrus TV-1 Launch Report
Jan.26/02
- Rocket Construction
Aug. 26/01
- Fins for Rocket Stability
Aug. 26/01
- Construction of a Rocket Fuselage using sheet aluminum
- Fuselage Structural Strength
- Launch Support System
Mar. 18/00
- Radio Transmitter
Recovery system
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- Rocket Recovery System Timer
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- Air-Speed Triggering System for Parachute Deployment
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- Rocket Altimeter System
- Parachute Recovery System
Mar.12/99
- Parachute Design and Construction
May 18/02
- Parts List (parachute construction)
- Parachute Structural and Drag Testing
June 30/01
Theory
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- Introduction to SRM Theory
- Basic Assumptions
- Propellant Grain
- Propellant Combustion
- Nozzle Theory
- Motor Thrust
- Motor Impulse
- Chamber Pressure
- Two-Phase Flow
- Corrections for Actual Rocket Motors
- GUIPEP Propellant Performance Software
- Theory Appendices
Miscellaneous
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- Construction of a Balance Scale for precision weighing
June 21/01
- Experimental Reports
Mar.2/02
- Technical Notepad #1
Apr.22/01
- Technical Notepad #2
- Technical Notepad #3
- Technical Notepad #4
- Downloads
- Links to over 100 NASA Space Vehicle Design (SP8000) Reports
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Contact address:
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371 Orton Park Road, Unit 52
Toronto, Ontario
Canada M1G 3V1
or If you have any questions or comments,
feel free to send me e-mail at
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Reports of broken links or viewing, graphics, & downloading problems are much appreciated !
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This site last updated January 1, 2005
Originally posted July 1997
Visitors to my website since Creation
"A man's reach should exceed his grasp...else, what's the heavens for?"