Propulsion Subsystem Functional Test Sample Clauses

Propulsion Subsystem Functional Test. 6-7 6.1.3 Initial Performance Test................................6-7 6.1.4 Ground Equipment Compatibility (PFM Only)...............6-8 6.2 THERMAL VACUUM TEST..............................................6-8 6.2.1 Pre-Thermal Vacuum Performance Test.....................6-8 6.2.2 Protoflight Spacecraft Thermal Testing..................6-8 6.2.3 Flight Acceptance Spacecraft Thermal Testing...........6-10 USE OR DISCLOSURE OF THE DATA CONTAINED ON THIS SHEET IS SUBJECT TO THE RESTRICTION ON THE TITLE PAGE.
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Propulsion Subsystem Functional Test. 6.1.3 INITIAL PERFORMANCE TEST * USE OR DISCLOSURE OF THE DATA CONTAINED ON THIS SHEET IS SUBJECT TO THE RESTRICTION ON THE TITLE PAGE.

Related to Propulsion Subsystem Functional Test

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  • Specification Changes (a) During the Term, GSK will accept a labeling change from Prometheus as contemplated by this Section 4.2 but otherwise the Parties acknowledge and agree that GSK does not intend to make any material changes (such as packaging design, manufacturing process or similar or related changes) to the existing Product during the Term.

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