ALLIANT TECHSYSTEMS OPERATIONS LLC

Federal contract awards won by ALLIANT TECHSYSTEMS OPERATIONS LLC (UEI TM7JBC68DDF3), 2016–2019 — public record from USAspending.

Showing awards of $250K+ active within the last 5 years. Need older history or smaller awards? Tell us what you need — we expand by request.

3
awards
$16,363,628
total value
2
agencies

Agencies buying from ALLIANT TECHSYSTEMS OPERATIONS LLC

National Aeronautics and Space Administration (2)Department of Defense (1)

What ALLIANT TECHSYSTEMS OPERATIONS LLC sells

541712 — RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES (EXCEPT BIOTECHNOLOGY) (2)336415 — GUIDED MISSILE AND SPACE VEHICLE PROPULSION UNIT AND PROPULSION UNIT PARTS MANUFACTURING (1)

Awards

ADVANCED INLET FOR HYPERSONIC AIRBREATHING PROPULSION
Department of Defense · $3,992,372 · Sep 23, 2019
IGF::OT::IGF8 FOOT HIGH TEMPERATURE TUNNEL MACH 6 NOZZLE. THE SCOPE OF THIS TASK ORDER IS TO PROCURE ALL MATERIALS AND HARDWARE REQUIRED FOR THE FABRICATION OF THE M6N AND TO FABRICATE THE NOZZLE BASED ON THE COMPLETED AND APPROVED DESIGN PRODUCED UNDER SMAAART CONTRACT NNL10AA05B, TASK NNL15AB92T. THE NOZZLE HARDWARE TO BE FABRICATED IS DEPICTED IN FIGURE 1 (EXHIBIT A OF THE STATEMENT OF WORK [SOW]). DRAWINGS OF THE NOZZLE COMPONENTS ARE INCLUDED AS AN ATTACHMENT TO THE SOW. THE NOZZLE CONSISTS OF COMPONENTS DENOTED AS PRESSURE VESSELS AND LINERS. THE LINERS ARE THE ACTIVELY COOLED COMPONENTS THAT FORM THE NOZZLE INTERNAL FLOW PATH. THE PRESSURE VESSELS ARE THE COMPONENTS INTO WHICH THE LINERS ARE ASSEMBLED. THE PRESSURE VESSELS SHALL BE AMERICAN SOCIETY OF MECHANICAL ENGINEERS (ASME) CODE STAMPED COMPONENTS RATED FOR THE MAXIMUM EXPECTED PRESSURE AND TEMPERATURE CONDITIONS POSSIBLE IN EACH NOZZLE SECTION. THE FABRICATED NOZZLE COMPONENTS SHALL MEET THE REQUIREMENTS OF LPR1710.40 REV M, LANGLEY RESEARCH CENTER PRESSURE SYSTEMS HANDBOOK, LPR1710.15 REV J, WIND TUNNEL MODEL SYSTEMS CRITERIA, AND THE ASME BOILER AND PRESSURE VESSEL CODE (LATEST REVISION), AS APPLICABLE.
National Aeronautics and Space Administration · $9,589,904 · Oct 2, 2017
IGF::CT::IGF THE EUROPA SOLID MOTOR BREAKING STAGE CHARACTERIZATION IS THE REQUIREMENT TO PROVIDE ENGINEERING SUPPORT TO THE DE-ORBIT STAGE OF THE LANDER. THIS REQUIREMENT INVOLVES CONTINUED MATURATION OF THE DE-ORBIT STAGE OF THE LANDER VEHICLE AS ALREADY BEGUN BY JPL PROPULSION PERSONNEL. THE OBJECTIVE IS TO COMPLETE PRELIMINARY STUDIES AND ANALYSIS ON THE FEASIBILITY OF A SOLID PROPULSION SYSTEM TO MEET THE NOTIONAL FLIGHT DEMANDS IN SUPPORT OF THE EUROPA PROGRAM.
National Aeronautics and Space Administration · $2,781,352 · Oct 27, 2016

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