PLASMA PROCESSES, LLC

Federal contract awards won by PLASMA PROCESSES, LLC (UEI KAWTP8XNFEK9), 2017–2026 — 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.

13
awards
$151,014,157,366
total value
2
agencies

Agencies buying from PLASMA PROCESSES, LLC

National Aeronautics and Space Administration (7)Department of Defense (6)

What PLASMA PROCESSES, LLC sells

541715 — RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES (EXCEPT NANOTECHNOLOGY AND BIOTECHNOLOGY) (11)541519 — OTHER COMPUTER RELATED SERVICES (1)541712 — RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES (EXCEPT BIOTECHNOLOGY) (1)

Awards

THE CONTRACTOR SHALL PROVIDE ALL NECESSARY MATERIALS, LABOR, EQUIPMENT AND FACILITIES INCIDENTAL TO THE PERFORMANCE OF THIS REQUIREMENT IN ACCORDANCE WITH THE TERMS OF THE ORDER.
Department of Defense · $151,000,000,000 · Jan 21, 2026
E014042 SBIR PHASE III CHEMICAL PROPULSION MODULE FOR THE GREEN PROPULSION DUAL MODE PROJECT
National Aeronautics and Space Administration · $872,381 · May 9, 2023
E014049 -100MN THRUSTER ENHANCEMENT PROGRAM
National Aeronautics and Space Administration · $383,507 · Dec 13, 2022
DEMONSTRATION OF LONG LIFE 1N THRUSTERS WITH ASCENT AND OTHER AF-M315 FORMULATIONS
Department of Defense · $765,429 · Dec 7, 2021
MULTI-USE COATING FOR ABRASION PREVENTION, WEAR PROTECTION, AND LUNAR DUST REMOVAL
National Aeronautics and Space Administration · $250,000 · Jun 2, 2021
DUAL MODE GREEN MONOPROPELLANT PROPULSION SYSTEM FOR INTERPLANETARY MISSIONS
National Aeronautics and Space Administration · $749,999 · Jan 15, 2021
REFRACTORY METAL COATED URANIUM NITRIDE FUEL FOR NUCLEAR THERMAL PROPULSION
National Aeronautics and Space Administration · $750,000 · Jun 19, 2020
RESEARCH&DEVELOPMENT LOW THERMAL CONDUCTIVITY VALVE FOR HIGHLY MANEUVERABLE UPPER STAGE MOTORS
Department of Defense · $2,964,686 · May 1, 2020
LUNAR FLASHLIGHT PROPULSION SYSTEM (LFPS) 100 MN THRUSTER
National Aeronautics and Space Administration · $988,064 · Dec 19, 2019
CARBON / CARBON COMPOSITE LEADING EDGES WITH INTEGRATED OXIDATION PROTECTION COATINGS FOR HYPERSONIC WEAPONS.
Department of Defense · $3,000,000 · Jun 17, 2019
SBIR PHASE II R&D; HIGHLY VECTORABLE, MULTI-PULSE ROCKET MOTOR NOZZLE TO ENHANCE MANEUVERABILITY OF ADVANCED INTERCEPTORS
Department of Defense · $989,443 · May 17, 2019
SBIR/STTR PHASE II R&D: COMPOSITE HOT STRUCTURES WITH OXIDATION PROTECTION
Department of Defense · $1,693,857 · Feb 11, 2019
IGF::OT::IGF NUCLEAR THERMAL PROPULSION (NTP) HAS BEEN IDENTIFIED AS A CRITICAL TECHNOLOGY NEEDED FOR HUMAN MISSIONS TO MARS AND BEYOND DUE TO ITS INCREASED SPECIFIC IMPULSE (ISP) AS COMPARED TO TRADITIONAL CHEMICAL PROPULSION SYSTEMS. RECENTLY, THE GAME CHANGING DEVELOPMENT (GCD) PROGRAM, WHICH IS A PARTNERSHIP BETWEEN NASA, DOE, AND INDUSTRY, WAS INITIATED TO EVALUATE THE FEASIBILITY OF A LOW ENRICHED URANIUM (LEU) NTP SYSTEM. A CRITICAL ASPECT OF NTP IS TO DEVELOP A ROBUST, STABLE FUEL. ONE OF THE FUEL CONFIGURATIONS CURRENTLY BEING EVALUATED IS A W-UO2 CERMET. FABRICATION OF FULL-SIZE CERMET ELEMENTS (>20?) HAS PROVEN TO BE DIFFICULT. AS A RESULT, THE USE OF CERMET SEGMENTS TO PRODUCE A FULL-SIZE FUEL ELEMENT IS OF INTEREST. HOWEVER, TECHNIQUES FOR JOINING THE SEGMENTS ARE NEEDED. DURING PHASE I, DIFFUSION BONDING TECHNIQUES WERE DEVELOPED FOR PRODUCING FUEL ELEMENTS FROM CERMET SEGMENTS. MICROSCOPIC EXAMINATION AND PRELIMINARY PROPERTIES TESTING SHOWED EXCELLENT JOINTS WERE FORMED. FOR EXAMPLE, QUANTITATIVE TENSILE TESTING OF W SAMPLES PRODUCED AT 1500C HIP WITH A NB INTERFACIAL COATING SHOWED THE FAILURES WERE IN THE BULK W AND NOT AT THE NB-W INTERFACES. THEREFORE, THE STRENGTH OF THE JOINTS WERE GREATER THAN THE STRENGTH OF THE BULK W MATERIAL. USING THE MOST PROMISING FABRICATION METHODS, A 6.3' LONG SIMULATED CERMET FUEL ELEMENT COMPRISED OF TWENTY-FIVE 0.25' THICK SEGMENTS WAS PRODUCED TO DEMONSTRATE PROOF-OF-CONCEPT. DURING THE PHASE II INVESTIGATION, THE HIP DIFFUSION BONDING PROCESS WILL BE OPTIMIZED FOR MAKING W CERMET BASED FUEL ELEMENTS. THIS WILL BE ACCOMPLISHED BY PERFORMING A PROCESS PARAMETER-CHARACTERIZATION-PROPERTIES STUDY. THE OPTIMIZED FABRICATION METHODS WILL THEN BE USED TO MAKE PROTOTYPE FUEL ELEMENTS WITH W CLADDINGS AND SUBSCALE FUEL ELEMENTS FOR DELIVERY TO NASA FOR HOT HYDROGEN TESTING
National Aeronautics and Space Administration · $750,000 · Apr 19, 2017

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