Phase I System
and Subsystem Testing

NOTE: The content of this page is being written as quickly as possible,
and each item will be posted as it is finished.

Test	Description and Type	Date	Location
1A-9b	Mx1-L-4 Engine Performance Test	June 21, 2002	Lockheed Martin
1A-9a	Mx1-L-3 Engine Performance Test	June 21, 2002	Lockheed Martin
	Test Report
	Drawings
	Raw Data
	Pictures
1A-8b	Lox System 1200 psi Hydrostatic Qualification Test	June 12, 2002	CU Durney Lab
	Test Report
	Pictures
1A-8a	Lox System 880 psi Hydrostatic Qualification Test	June 10, 2002	CU Durney Lab
	Test Report
	Pictures
1A-7	Lox System Cryogenic Flow Performance and Qualification Test	June 8, 2002	CU Durney Lab
	Test Report
	Raw Data
	Pictures
1A-5d	Lox System Water Flow Qualification Test	June 4, 2002	CU Durney Lab
	Test Report
	Raw Data
	Pictures
1A-6	Sparker 1200 psi Hydrostatic Qualification Test	June 26, 2002	CU Durney Lab
	Test Report
	Pictures
1A-5a,b,c	Lox System Water Flow Performance Tests	May 21, May 20, 2002	CU Durney Lab
	Test Report
	Raw Data
	Pictures
1A-4	Injector Performance Determination Tests	April 06, 2002	CU Durney Lab
	Test Report
	Raw Data
	Pictures
1A-3b	6-Hole Igniter Ignition Performance Test	March 26, 2002	CU
	Test Report
	Pictures
1A-2b	Chamber 2 1000 psi Hydrostatic Qualification Test	March 17, 2002	CU ITLL
	Test Report
	Pictures
1A-3a	4-Hole Igniter Ignition Performance Test	March 02, 2002	CU
	Test Report
	Pictures
1A-2a	Chamber 1 1000 psi Hydrostatic Qualification Test	November 27, 2001	CU ITLL
	Test Report
	Pictures
1A-1a to 1A-1p	Fuel Grain CompositionTests	October 01 to January 2002	CU ITLL
	Test Report
	Pictures