|Predecessor||Estes Industries, Estes-Cox Corp.|
|Founded||Denver, Colorado, U.S. (1958 )|
|Products||Model rockets and Model aircraft|
Estes Industries (aka Estes-Cox Corp.) is a company that was started in Denver, Colorado, USA. The company was the first to mass-produce model rocket engines with consistent and reliable performance. The company soon began producing model rocket kits, launch equipment and other accessories. In 1961, the company was moved to a 77-acre tract of land on the outskirts of Penrose, Colorado. Rapid growth followed and soon Penrose became known as the "Model Rocket Capital of the World". In 1969 Vernon Estes sold the company to the Damon Corporation of Needham Hts, MA. Damon purchased a number of other hobby companies including a smaller competitor of Estes, Centuri Engineering of Phoenix, AZ. Damon merged the two companies under the name Centuri Engineering. The Penrose entity continued doing business as Estes Industries. Centuri Engineering model rocket products continued to be developed, marketed and sold from the Centuri offices in Phoenix as well, although the actual manufacturing of Centuri products was soon moved to the Estes facility in Penrose, CO. Sales of Centuri model rocket products were never as successful as Estes brand products and the Centuri Engineering offices in Phoenix were finally closed and the Centuri product line was discontinued in 1983.
Following a hostile takeover of the Damon Corporation in 1989, Estes Industries was divested and became part of Hobby Products. The business name of the company was shortened to Centuri Corporation. In 1996 Hobby Products acquired the assets of Cox Products of Corona, CA. Cox Products was a designer and manufacturer of model airplanes and glow-fuel model airplane engines and more. The company’s assets were moved to the Estes facility. In 2002, the combined company was sold again and the company’s name was changed to Estes-Cox Corp.
On January 15, 2010 Estes-Cox was again sold and became a wholly owned subsidiary of Hobbico of Illinois. Sales of the Cox line of model airplanes has been continued by Hobbico.
Estes Industries was founded by Vernon Estes in 1958. In 1969 Vernon Estes sold the company to the Damon Corporation. On August 30, 2002, Barry Tunick, who had been the Chief Executive Officer since 1991, acquired Estes-Cox Corporation from the private equity fund, TCW Capital, for the sum of $15 million. On January 15, 2010, Estes-Cox was acquired by Hobbico, Inc.
Vern Estes created "Mabel". "Mabel" was a machine designed to safely and inexpensively manufacture model rocket engines for Model Missiles Incorporated. Mabel was capable of producing a completed model rocket engine every 5-1/2 seconds. The operation began with an engine casing tube being loaded onto a rotating table. The table then advances through multiple stations where the nozzle, propellant, delay and ejection components are added. A paper end cap is then cut from a roll of heavy paper tape and inserted to retain the loose ejection charge. The completed engine is then ejected from the table, sent through the printer and dropped into the finished engine box below.
Indoor launch of model rockets in Astrodome
Estes produced a wide variety of rocket model kits, normally using paperboard tubing for the fuselage and balsa wood for fins and nose cones. Early models tended to be relatively simple in design terms, differing in terms of size, number of stages and recovery method. One particularly well known design from this era was the Camroc, a small camera that replaced the nose cone of larger models that was designed to take a single image on a small disk of film when the motor had burned out and the rocket was facing downward. The Cineroc used a small movie camera that could be launched from larger rockets, taking a series of frames as the rocket ascended.
Later model kits from the late 1970s and early 1980s tended to be more for show than performance, including a series of scale or sport-scale designs and "exotics". Centuri was also well known for these sorts of designs, and the two companies often copied design elements from the other's latest models. The downturn in the hobby in the later 1980s led to consolidation of the two companies. During the 1990s the model line was dramatically reduced, and the ones that were left were typically very simple "three fins and a nose cone" designs that were partially or entirely preassembled.
Estes rocket engine color-coding
Estes engines are color-coded for recommended use.
- Green engines are for use in single-stage models.
- Purple engines for the top stages of multistage rockets and very light single-stage rockets.
- Red engines for all booster and intermediate states of multi-stage models.
- Blue are "plugged" and are used for rocket-powered racers, aerobrake recovery rockets, and radio controlled gliders; they contain no delay or ejection charge.
- Black has been used in the past for static test engines, which were also plugged to prevent blow-through.
It can be dangerous to use upper-stage engines in normal single-stage rockets. The large delay in ejection can be problematic. The rocket may already be halfway through its descent when the nose comes off and the rocket may not slow down enough before it hits the ground.
Estes number coding
|Type||Total Impulse (Newton seconds)|
Each rocket engine has a code printed upon the outer jacket. This code is defined by the National Association of Rocketry (NAR). An example of one such code is A8-3.
The capital letter (e.g., A) indicates total impulse produced by the engine. Each succeeding letter represents a power range with maximum total impulse twice the impulse of the previous letter. (Example: A single C engine can produce anywhere from 5.01 to 10 newton-seconds of impulse, a G engine 80.1 to 160 newton-seconds.) Anything over a G engine is considered high power model rocketry.
The first number (e.g., 8) specifies that engine's average thrust in newtons or the average push exerted by the engine. Thus a B6-0 and a C6-0 will both produce the same average thrust of 6 newtons, but the C6-0, having twice the total impulse, will fire for twice as long. The rocket engines produce maximum thrust shortly after ignition and thrust declines to a steady-state which is maintained for up to 2.5 seconds prior to burnout.
The final number (e.g., 3) indicates the delay between the thrust and the ejection charge, in seconds. Engines with a delay of zero are typically used as booster engines in multi-stage rockets and there is no ejection charge. In this case, the burning propellant ruptures through the top and hot bits of propellant enter the nozzle of the upper stage engine, thus igniting that engine and forcing the booster assembly away, hopefully to tumble safely to earth.
Estes engine construction
The solid propellant is ignited by a coated wire inserted through the nozzle and in contact with the propellant. An electric current heats the wire and ignites the solid propellant. An engine can also be ignited by the hot gases from the propellant of a booster engine.
Estes model rockets are popular and used by a large number of hobbyists and educators. However, measurements reported by a group at the University of Central Arkansas found that Estes rocket motor models A3-4T, A8-3, B4-4, B6-4, C6-5, and D12-3 have a measured impulses from 15.4% to 22.8% below the claimed impulse. A study at the Australian Defence Force Academy found Estes D11-P motor to have an impulse 11.4% below Estes specifications and the C6-0 motor to be 4.45% below Estes' specifications. A third study found the A10-PT motor to have a total impulse 20% below Estes' claims.
- "Hobbico acquires model rocket maker Estes-Cox" Champaign-Urbana News Gazette - January 2010
- "Vern Estes using Mabel".
- "Reference information about Mabel".
- Model Rocket News Volume 10, No 1 February 1970
- "Article in Model Rocket Man" (PDF).
- "Estes Engine Chart" (PDF).
- "Estes Model Rocket Engines, Engine Time/Thrust Curves" (PDF).
- Penn, Kim and William V. Slaton, Measuring Model Rocket Engine Thrust Curves, The Physics Teacher -- December 2010 -- Volume 48, Issue 9, pp. 591.
- An Investigation into the Combustion and Performance of Small Solid-Propellant Rocket Motors M.G. Carter. University of New South Wales at the Australian Defense Force Academy. 2008.
- Measuring thrust and predicting trajectory in model rocketry M. Courtney and A. Courtney. Cornell University Library. 2009.
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