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	<id>https://ssi-wiki.stanford.edu/w/api.php?action=feedcontributions&amp;feedformat=atom&amp;user=Blakehord</id>
	<title>Stanford SSI Wiki - User contributions [en]</title>
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	<updated>2026-05-11T14:39:55Z</updated>
	<subtitle>User contributions</subtitle>
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	<entry>
		<id>https://ssi-wiki.stanford.edu/w/index.php?title=Ortega&amp;diff=4128</id>
		<title>Ortega</title>
		<link rel="alternate" type="text/html" href="https://ssi-wiki.stanford.edu/w/index.php?title=Ortega&amp;diff=4128"/>
		<updated>2020-10-26T16:49:17Z</updated>

		<summary type="html">&lt;p&gt;Blakehord: Added more subsections&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;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. &lt;br /&gt;
&lt;br /&gt;
==Naming Convention==&lt;br /&gt;
===Ortega v1.0===&lt;br /&gt;
===Ortega v1.1===&lt;br /&gt;
===Ortega v2.0===&lt;br /&gt;
&lt;br /&gt;
==Design Parameters==&lt;br /&gt;
&lt;br /&gt;
==Engine Structure==&lt;br /&gt;
===Tanks===&lt;br /&gt;
===Propellant Manifold===&lt;br /&gt;
===Pyrovalves===&lt;br /&gt;
===Injector===&lt;br /&gt;
===Combustion Chamber===&lt;br /&gt;
===Nozzle===&lt;br /&gt;
&lt;br /&gt;
==Ground Support Equipment==&lt;br /&gt;
===eGSE===&lt;br /&gt;
===mGSE===&lt;br /&gt;
&lt;br /&gt;
==Testing History==&lt;br /&gt;
===Procedure===&lt;br /&gt;
===Hotfire #1===&lt;br /&gt;
===Hotfire #2===&lt;br /&gt;
&lt;br /&gt;
==Design Updates==&lt;br /&gt;
===Welded Tank Design===&lt;br /&gt;
======&lt;br /&gt;
&lt;br /&gt;
[[Category:Rockets]]&lt;/div&gt;</summary>
		<author><name>Blakehord</name></author>
	</entry>
	<entry>
		<id>https://ssi-wiki.stanford.edu/w/index.php?title=Ortega&amp;diff=4127</id>
		<title>Ortega</title>
		<link rel="alternate" type="text/html" href="https://ssi-wiki.stanford.edu/w/index.php?title=Ortega&amp;diff=4127"/>
		<updated>2020-10-26T16:44:52Z</updated>

		<summary type="html">&lt;p&gt;Blakehord: Created page and outline of contents&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;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. &lt;br /&gt;
&lt;br /&gt;
==Naming Convention==&lt;br /&gt;
===Ortega v1.0===&lt;br /&gt;
===Ortega v1.1===&lt;br /&gt;
===Ortega v2.0===&lt;br /&gt;
&lt;br /&gt;
==Design Parameters==&lt;br /&gt;
&lt;br /&gt;
==Structure==&lt;br /&gt;
===Tanks===&lt;br /&gt;
===Propellant Manifold===&lt;br /&gt;
===Pyrovalves===&lt;br /&gt;
===Injector===&lt;br /&gt;
===Combustion Chamber===&lt;br /&gt;
===Nozzle===&lt;br /&gt;
&lt;br /&gt;
==Ground Support Equipment==&lt;br /&gt;
&lt;br /&gt;
==Testing History==&lt;br /&gt;
===Procedure===&lt;br /&gt;
===Hotfire #1===&lt;br /&gt;
===Hotfire #2===&lt;br /&gt;
&lt;br /&gt;
==Design Updates==&lt;br /&gt;
&lt;br /&gt;
[[Category:Rockets]]&lt;/div&gt;</summary>
		<author><name>Blakehord</name></author>
	</entry>
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