Difference between revisions of "Ortega"
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==Design Parameters== | ==Design Parameters== | ||
| − | ==Structure== | + | ==Engine Structure== |
===Tanks=== | ===Tanks=== | ||
===Propellant Manifold=== | ===Propellant Manifold=== | ||
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==Ground Support Equipment== | ==Ground Support Equipment== | ||
| + | ===eGSE=== | ||
| + | ===mGSE=== | ||
==Testing History== | ==Testing History== | ||
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==Design Updates== | ==Design Updates== | ||
| + | ===Welded Tank Design=== | ||
| + | ====== | ||
[[Category:Rockets]] | [[Category:Rockets]] | ||
Latest revision as of 16:49, 26 October 2020
Ortega is a bipropellant liquid rocket engine spun out of the Helios Project for flight at IREC. It uses nitrous oxide as an oxidizer and kerosene as a fuel. It has been hotfired twice, but has not been flown yet.