22.03.2013 Views

OTRAG Rocket.pdf

OTRAG Rocket.pdf

OTRAG Rocket.pdf

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

<strong>OTRAG</strong> injection head in the first phase of the project until 1972, there were already 200<br />

firing tests with 3 failures. By the end of the support by the BMFT, in 1974 there were<br />

2,000 tests and now it will be 6000, with an accumulated operating time of 1 million<br />

seconds. I have received from Lutz Kayser no slice of the engine, fearing that someone<br />

might steal his intellectual property. The pictures here show, therefore, only the<br />

schematic operation.<br />

Each engine has an overhead line from the oxidizer and fuel tank. Unlike other engines,<br />

the fuel injection is not a head above the engine but is injected radially from the outside.<br />

Lutz Kayser points this out as one of 31 developments that worked only after long time<br />

and some setbacks. The injection is performed by 3 rings with 144 holes, which should<br />

allow a particularly good combination. The radial approach prevents the fuel reaches the<br />

combustion chamber wall, and thus cut off the reaction. The result is a very high<br />

combustion efficiency. The nozzle throat is a simple graphite ring. Due to its opening, the<br />

thrust will be regulated in a very wide range. The engine is so varied in a wide range of 5-<br />

50 kN. An aperture of 80 mm was used in the tests with 6 or 12 m long modules. This

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!