• ⌘ + K
  • Home
  • 0
    Inbox
Explore
  • Browse All
  • Health
  • FedCiv
  • Defense
  • Events
Work
  • Teaming Hub
  • Watchlists
  • Bookmarks
  • Notes
Research
  • Grants
    • Contracts
    • Vehicles
    • OTAs
    • OTIDVs
  • Agencies
  • NAICS
  • PSC
  • DOGE Tracker

Federal Contract Awards

105awards

Analyze awards, watch incumbents and competitors, track new transactions or changes, and use award history to shape recompete and capture strategy.

PSC Codes
is
Award ID
Description
Recipient
Total Value
Awarding Agency
Funding Agency
Set Aside
NAICS
PSC
Award Date
Start Date
End Date
NNM12AA23C
STTR PHASE III AWARD DEVELOPMENT OF ROBUST, PRODUCTION QUALITY WATER MITIGATION MODEL IN LOCI\CHEM STATEMENT OF WORK 1. BACKGROUND NASA/MSFC HAS A NEED FOR A CFD-BASED MODEL OF WATER MITIGATION FOR ROCKET VEHICLE LAUNCH PAD ENVIRONMENTS. APPLICATION OF LIQUID WATER ON THE LAUNCH PAD IS USEFUL FOR SUPPRESSION OF IGNITION OVER PRESSURE (IOP) AND LAUNCH PAD ACOUSTIC ENVIRONMENTS. TRADITIONALLY, WATER IS APPLIED IN LARGE QUANTITIES TO LOCATIONS CONCENTRATED NEAR THE ROCKET ENGINE OR MOTOR NOZZLE EXIT PLANE IN ORDER TO SUPPRESS THE PRESSURE AND THERMAL LOADS ON THE ROCKET VEHICLE AND LAUNCH PAD GENERATED BY THE ENGINE OR MOTOR START TRANSIENT. WATER IS ALSO SUPPLIED IN A LESS CONCENTRATED MANNER TO THE SURFACES WHERE THE ENGINE OR MOTOR PLUMES IMPINGE ON THE LAUNCH PAD IN ORDER TO SUPPRESS THE ACOUSTIC LOAD IMPOSED UPON THE ROCKET VEHICLE. THE SELECTION OF THE WATER APPLICATION LOCATIONS AND QUANTITIES ARE HISTORICALLY GUIDED BY THE RESULTS OF EXPERIMENTS CONDUCTING USING SUBSCALE ROCKET ENGINES AND MOTORS ALONG WITH A SUBSCALE LAUNCH PAD. THESE SUBSCALE EXPERIMENTS ARE EXPENSIVE AND TIME-CONSUMING. COMPUTATIONAL FLUID DYNAMICS (CFD) -BASED METHODS TO AUGMENT THE DESIGN PROCESS WOULD BE A WELCOME DEVELOPMENT. NASA/MSFC HAS RECENTLY VALIDATED THE LOCI\CHEM CFD PROGRAM FOR THE PREDICTION OF SUBSCALE ROCKET MOTOR IOP ENVIRONMENTS FOR CONDITIONS WHERE WATER MITIGATION IS NOT PRESENT. THE LAGRANGIAN PARTICLE MODEL IN LOCI\CHEM HAS ALSO BEEN USED IN ATTEMPTS TO PREDICT THE EFFECTS OF WATER ADDITION IN LOCATIONS SELECTED TO MITIGATE BOTH IOP AND ACOUSTIC ENVIRONMENTS. WHILE THESE MODELS HAVE RESULTED IN PHYSICALLY-REALISTIC ALTERATIONS OF THESE ENVIRONMENTS, THE SIMULATIONS HAVE NOT BEEN RUN TO COMPLETION DUE TO A SEVERE LACK OF ROBUSTNESS. THE CORE CAUSE OF THE LACK OF ROBUSTNESS APPEARS TO ORIGINATE FROM CONDITIONS DEVELOPING WHICH VIOLATE THE BASIC JUSTIFYING APPROXIMATIONS BEHIND THE LAGRANGIAN PARTICLE MODEL. IN CFD SIMULATIONS, LARGE NUMBERS OF PARTICLES ACCUMULATE IN CERTAIN REGIONS, TYPICALLY NEAR SOLID SURFACES, LEADING TO THE RATIO OF PARTICULATE PHASE TO GASEOUS PHASE MASS BECOMING LARGE ENOUGH TO VIOLATE THE DISPERSED ASSUMPTION BEHIND THE PARTICLE MODEL FORMULATION AND LEADING TO A NUMERICAL INSTABILITY IN THE SOLUTION OF THE COUPLED GAS PHASE/PARTICULATE SYSTEM OF EQUATIONS. A NEED EXISTS TO INVESTIGATE THE CAUSES OF THE LACK OF ROBUSTNESS DESCRIBED ABOVE AND FORMULATE APPROACHES WHICH LEAD TO SUCCESSFUL, ROBUST SIMULATIONS AND VALIDATION OF PREDICTIONS OF WATER MITIGATION FOR IOP AND ACOUSTIC ENVIRONMENT GENERATION ON ROCKET VEHICLE LAUNCH PADS. 2. SCOPE A RECENTLY AWARDED STTR PHASE II CONTRACT NNX12CB09C, ADVANCED FLOW ANALYSIS TOOLS FOR TRANSIENT SOLID ROCKET MOTOR SIMULATIONS , WAS AIMED AT IMPROVING THE IGNITION MODELING AND GRAIN RECESSION OF SOLID ROCKET PROPELLANTS INCLUDING THE SOLID PARTICLES GENERATED AT THE COMBUSTING FUEL SURFACE AND PROPAGATED OUT OF THE ROCKET USING THE LAGRANGIAN PARTICLE MODEL. THIS EFFORT BUILDS UPON A PREVIOUS STTR PHASE I AND PHASE II CONTRACT, NNX09CB73C, MULTI-PHASE FLOW ANALYSIS TOOLS FOR SOLID MOTOR APPLICATIONS , WHICH DEVELOPED SOLID PARTICLE TO WALL INTERACTION MODELS USING THE LAGRANGIAN PARTICLE MODEL. IN ADDITION, THIS CONTRACT ALSO DEVELOPED CHARACTERIZATIONS OF THE MIXED-PHASE THERMODYNAMICS AND SHOCK PROPAGATION. THIS WORK EFFORT SHALL CHARACTERIZE AND DIAGNOSE THE SEQUENCE OF EVENTS LEADING TO THE ULTIMATE LACK OF ROBUSTNESS OF LAGRANGIAN PARTICLE MODEL-BASED CFD SIMULATIONS OF LIQUID WATER APPLICATION TO ROCKET VEHICLE LAUNCH PADS. BASED ON THIS CHARACTERIZATION, IMPROVEMENTS, ADDITIONS AND/OR ALTERATIONS TO THE LOCI\CHEM CFD PROGRAM AND LAGRANGIAN PARTICLE MODEL SHALL BE FORMULATED AND IMPLEMENTED TO REMEDY THE LACK OF ROBUSTNESS.TETRA RESEARCH CORPORATION$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541511Custom Computer Programming ServicesAR44Sep 11, 2012Sep 11, 2012Dec 11, 2013
NNM12AA22C
IGF::CL::IGF SBIR PHASE III- PC- SIGNAL HIGH FREQUENCY DATA DIAGNOSTICS.AI SIGNAL RESEARCH INC$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541712AR44Sep 5, 2012Sep 1, 2012Aug 31, 2014
SMD70011M0218
BIOMETRIC DATA COLLECTION DEVICES (2 UNITS)(PO)MISCELLANEOUS FOREIGN AWARDEES$15,436STATE, DEPARTMENT OFSTATE, DEPARTMENT OF—333612Speed Changer, Industrial High-Speed Drive, and Gear ManufacturingAR44Mar 16, 2011Mar 16, 2011Mar 16, 2011
GS02P08PKP0141
INSTALLING THE CAT 6 CABLING TO ROOM 605.J & R TELECOMMUNICATIONS INC$6,619PUBLIC BUILDINGS SERVICE——541519Other Computer Related ServicesAR44May 14, 2008May 14, 2008Jul 31, 2008
NNG08DA00C
THIS CONTRACT IS TO DESIGN, DEVELOP, FABRICATE, INTEGRATE, TEST, SHIP, PROVIDE LAUNCH SUPPORT, CONDUCT ON-ORBIT CHECKOUT OPERATIONS AND PROVIDE SUSTAINING ENGINEERING SUPPORT FOR TWO TRACKING DATA RELAY SATELLITE (TDRS) SPACECRAFT. THE CONTRACT REQUIREMENTS ALSO INCLUDE THE DESIGN, ASSEMBLE, TEST, INSTALL AND VERIFICATION OF MODIFICATIONS TO THE WHITE SANDS COMPLEX NECESSARY TO MAKE THE GROUND TERMINALS FULLY COMPATIBLE WITH THE TDRS K PROGRAM SPACECRAFT DESIGN. THE CONTRACT ALSO INCLUDES OPTIONS FOR TWO ADDITIONAL SPACECRAFT.THE BOEING COMPANY$1,255,899,177NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541330Engineering ServicesAR44Dec 28, 2007Dec 28, 2007Feb 5, 2026
FA920007C0229
MISSILE WARNING SYSTEM DEMONSTRATIONDOPPLERTECH, INC.$116,247DEPT OF THE AIR FORCEDEPT OF THE AIR FORCE—541330Engineering ServicesAR44Jun 6, 2007Jun 6, 2007Aug 3, 2007
NNA07BB12P
SAP PURCHASE REQUISITION: 4200188087 SENSORWARE SYSTEMS WILL PROVIDE DESIGN ADVICE AND ENGINEERING SPECIFICATIONS TO ENSURE THAT THE DEVELOPED SENSORS ARE PRACTICAL FROM BOTH AN ENGINEERING AND OPERATIONS STANDPOINT FOR BOTH NASA AMES AND THE TECHNICAL SUPPORT WORKING GROUP.SENSORWARE SYSTEMS INC$8,000NATIONAL AERONAUTICS AND SPACE ADMINISTRATION——541990All Other Professional, Scientific, and Technical ServicesAR44Mar 8, 2007Mar 8, 2007May 28, 2007
NNC07CA45C
SAP PURCHASE REQUISITION: 4200177011 FABRICATION, DELIVERY AND TEST OF TEN URFC STACK AND FABRICATION, DELIVERY AND TEST OF TEN CELL STATIC FEED FUEL CELLPROTON ENERGY SYSTEMS INC$150,000NATIONAL AERONAUTICS AND SPACE ADMINISTRATION——541710AR44Dec 7, 2006Dec 7, 2006Dec 1, 2007
NNA06BB90T
RISK ASSESSMENT FOR AERONAUTICS AND EXPLORATION SYSTEMSVALADOR INC$134,586NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541611Administrative Management and General Management Consulting ServicesAR44Sep 25, 2006Sep 20, 2006Dec 30, 2007
NNJ04JG98I
ENGINEERING SUPPORT INCLUDING TRAVELUS AIR FORCE$6,000NATIONAL AERONAUTICS AND SPACE ADMINISTRATION———AR44Jun 8, 2004Jun 8, 2004Sep 30, 2004
GSFC0200101DNAS500118
SUSTAINING ENGINEERING SUPPORT SERVICESL3 TECHNOLOGIES, INC.$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATION——541330Engineering ServicesAR44Jan 15, 2001Jan 15, 2001Apr 30, 2009
MSFC0199905DNAS899113
DESIGN AND FABRICATION OF HYDRAULIC DUMP INTERFACE SYSTEMALPHA TECHNOLOGY INC$367,709NATIONAL AERONAUTICS AND SPACE ADMINISTRATION———AR44May 7, 1999May 7, 1999Sep 30, 2002
MSFC0199709BH28904D
—LOCKHEED MARTIN CORP$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATION———AR44Sep 15, 1997Sep 15, 1997Nov 15, 1997
MSFC0199708DH28627D
—ELECTRIC PROPULSION LABORATORY, INC.$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATION———AR44Aug 15, 1997Aug 15, 1997Oct 15, 1997
MSFC0199707DH28628D
—TRITON SYSTEMS, INC.$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATION———AR44Jul 15, 1997Jul 15, 1997Feb 15, 1998
GSFC0199705BS85239Z
—EUREKA SCIENTIFIC, INC.$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATION———AR44May 15, 1997May 15, 1997Oct 15, 1997
F0470190C0009
199712!5700!0019!GZ46 !SMC/PKG DIR SPACE NAV SYS CONT !F0470190C0009 !A!*!P00085 !19961212!19970114!874543135!931114334!834951691!N!4N497!LOCKHEED MARTIN CORPORATION !700 N FREDERICK AVE !GAITHERSBURG !MD!20879!31175!031!24!GAITHERSBURG !MONTGOMERY !MARYLAND !0001!+000000521650!N!N!000000000000!AR44!RDTE/SPACE OP - TRACKING & DATA ACQ-DEMO/VALID !A2 !MISSILE AND SPACE SYSTEMS !3GAJ!NAVSTAR !3761!3!*!*!C!B!A!*!A !N!R!2!005!B!* !A!Y!Z!* !* !N!C!*!C!C!A!A!A!*!* !*!N!A!C!N!*!*!*!*!*!LOCKHEED MARTIN CORPORATION$0DEPT OF THE AIR FORCE———AR44Dec 12, 1996Dec 12, 1996—
JSC00198909DNAS918243
—INTERNATIONAL BUSINESS MACHIN$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATION———AR44Sep 15, 1996Sep 15, 1996Sep 15, 1991
ARC00199505DNAS214256
LUNAR PROSPECTORLOCKHEED MISSILES & SPACE COMP$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATION———AR44May 15, 1995May 15, 1995Aug 25, 2005
GSFC0199007DNAS530927
—UNIVERSITY SYSTEM OF MARYLAND$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATION——541710AR44Jan 15, 1995Jan 15, 1995Apr 15, 1995
GSFC0199409BNAS532638
—ELECTROLOGIC OF AMERICA$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATION———AR44Sep 15, 1994Sep 15, 1994Sep 15, 1994
GZ460199409BF0470190C0009
—LOCKHEED MARTIN CORPORATION$0DEPT OF THE AIR FORCE———AR44Sep 15, 1994Sep 15, 1994Dec 15, 1996
GSFC0199408BNAS532638
—ELECTROLOGIC OF AMERICA$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATION———AR44Aug 15, 1994Aug 15, 1994Sep 15, 1994
GSFC0199408BNAS530927
—UNIVERSITY SYSTEM OF MARYLAND$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATION———AR44Aug 15, 1994Aug 15, 1994Nov 15, 1994
GSFC0199407DNAS532638
—ELECTROLOGIC OF AMERICA$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATION———AR44Jul 15, 1994Jul 15, 1994Dec 15, 1994
Page 1 of 5
  • Previous
  • Next