Average obligated amount per year since period start.
Portion of total contract value already obligated.
Share of total value represented by subawards.
TWO CARBON-OVERWRAP ABLATIVE THRUST CHAMBER/NOZZLE ASSEMBLIES FOR A LOX/METHANE COMBUSTOR. SPLIT SYSTEM WITH TWO PARTS: A CARBON OVERWRAP ABLATIVE CHAMBER/NOZZLE ENDING AT AR 9, AND A NOZZLE EXTENSION STARTING AT AR 10.5 AND ENDING AT A TOTAL AR OF 100. AT THE JOINT, JSC WILL ADD A FLANGED HELIUM HEAT EXCHANGER. JSC WILL SUPPLY THE INJECTOR END, CHAMBER END, AND NOZZLE EXTENSION STAINLESS STEEL FLANGES. A SINGLE-PART THRUST CHAMBER ASSEMBLY WITH THE SAME OVERALL DIMENSIONS AS UNIT 1), WITHOUT A NOZZLE SEPARATION PLANE, BUT INCLUDING AN EMBEDDED HELIUM HEAT EXCHANGER. JSC WILL PROVIDE THE HELIUM HEAT EXCHANGER AND INJECTOR END FLANGE. BOTH UNITS NEED TO HAVE THE SAME THRUST CHAMBER AND NOZZLE GEOMETRY.
Task order obligations
Estimated months remaining until end of performance.
Period of performance
100% of period elapsed
Awarding Agency
NANATIONAL AERONAUTICS AND SPACE ADMINISTRATION
Code: 8000
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