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Award ID | Description | Recipient | Total Value | Awarding Agency | Funding Agency | Set Aside | NAICS | PSC | Award Date | Start Date | End Date | |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| SBIR PHASE III 80NSSC25C0444 IN-SPACE LOX/METHANE PINTLE PROPULSION ENGINE EVALUATION AND DEMONSTRATION | KT ENGINEERING CORPORATION | $405,908 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology) | AJ14GENERAL SCIENCE AND TECHNOLOGY R&D SERVICES; GENERAL SCIENCE AND TECHNOLOGY; R&D ADMINISTRATIVE EXPENSES | Sep 29, 2025 | Sep 30, 2025 | Aug 15, 2026 | ||
| ..IGF::OT::IGF SBIR/STTR PHASE II R&D | KT ENGINEERING CORPORATION | $1,098,820 | MISSILE DEFENSE AGENCY (MDA) | MISSILE DEFENSE AGENCY (MDA) | — | 541712 | AC22NATIONAL DEFENSE R&D SERVICES; ATOMIC ENERGY DEFENSE ACTIVITIES; APPLIED RESEARCH | Jan 10, 2017 | Jan 10, 2017 | May 9, 2019 | ||
| IGF::OT::IGF KTE'S PROPOSED INNOVATION IS THE LOX/METHANE PINTLE PROPULSION ENGINE OR (LMPPE), WHICH CAN OFFER HIGHER RELIABILITY, LOWER COST AND HIGHER PERFORMANCE THAN CONVENTIONAL IMPINGING INJECTOR-BASED COMBUSTION DEVICES FOR IN SPACE PROPULSION SYSTEMS. THE CONCEPT CAN BE USED IN BOTH PUMP AND PRESSURE-FED ENGINE ARCHITECTURES. THE LMPPE BUILDS UPON THE CATALYTICALLY INITIATED COMBUSTOR (CIC) IGNITER TECHNOLOGY PREVIOUSLY DEMONSTRATED TO A HIGH TRL COUPLED WITH A LOW COST PINTLE MAIN INJECTOR THAT HAS POTENTIAL TO PROVIDE A PATH FOR A LOX/METHANE UPPER STAGE ENGINE THAT IS DYNAMICALLY STABLE OFFERING HIGH PERFORMANCE WITH A WIDE THROTTLE CAPABILITY OVER A RANGE OF PROPELLANT INLET CONDITIONS. THE CIC BASED PINTLE PROPULSION ENGINE ALSO OFFERS ATTRACTIVE PACKAGING ADVANTAGES AND IMPROVED RELIABILITY AND OPERABILITY WHILE REDUCING DEVELOPMENT COSTS AND RISKS FOR UPPER-STAGE ENGINES. THE PINTLE PROPULSION APPROACH REQUIRES LOOSER TOLERANCES OF THE COMPONENTS AND CAN BE SUCCESSFULLY FABRICATED FROM A NUMBER OF ADDITIVE MANUFACTURING APPROACHES. THIS MULTI-FUNCTIONAL CAPABILITY WILL FURTHER REDUCE COST AND IMPROVE RELIABILITY IN LAUNCH OR IN-SPACE VEHICLES BY INCREASING COMPONENT PRODUCTION RATES AND REDUCING PART COUNT. THE FOCUS OF THE PROPOSED EFFORT IS TO PROVE THE FEASIBILITY OF THIS NOVEL OXYGEN/METHANE PINTLE ENGINE. THE IN-SPACE ENGINE CAN BE DESIGNED TO OPERATE AT LOWER CHAMBER PRESSURES, LENDING ITSELF TO THE USE OF COMPOSITE AND ADDITIVE MANUFACTURED COMPONENTS. THE DESIGN OFFERS AN INHERENT COMBUSTION STABILITY ALLOWING SIMPLER COMBUSTION CHAMBER DESIGNS AND EASE OF FABRICATION DUE TO THE OMISSION OF COMPLEX ACOUSTIC DAMPING DEVICES. THEREFORE, AN EXPENSIVE DEVELOPMENT PROGRAMS CAN BE AVOIDED DUE TO THE VERY LOW RISK OF COMBUSTION INSTABILITY. | KT ENGINEERING CORPORATION | $124,823 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCH | Jun 9, 2015 | Jun 17, 2015 | Dec 17, 2015 | ||
| IGF::OT::IGF KT ENGINEERING (KTE) IS PLEASED TO SUBMIT THIS SMALL BUSINESS INNOVATION RESEARCH (SBIR) PHASE III PROPOSAL. THIS PROPOSAL ADDRESSES A NEED FOR INNOVATIVE SOLUTIONS THAT WILL ALLOW FUTURE SPACEPORT LAUNCH SERVICE PROVIDERS TO OPERATE IN AN EFFICIENT, LOW COST MANNER. WE PROPOSE TO BUILD UPON THE SUCCESSFUL RESULTS OF OUR SBIR PHASE I EFFORT (REFERENCE CONTRACT NNX12CF02P) AND CONDUCT RESEARCH TO DEMONSTRATE FEASIBILITY OF A NOVEL LAUNCH VEHICLE PRESSURIZATION SYSTEM CONCEPT THAT WILL INCREASE PERFORMANCE AND RELIABILITY COMPARED WITH TRADITIONAL APPROACHES, REDUCE DEPENDENCE UPON HELIUM UP TO 50%, ENABLE THE USE OF LOW-COST COMMERCIAL-OFF-THE-SHELF (COTS) TECHNOLOGY, AND DEMONSTRATE AUTOMATED GROUND PROCESSING ASSOCIATED WITH PRESSURANT LOADING AND CONDITIONING. OUR INNOVATION IS BASED ON FIVE MAJOR TECHNOLOGY AND OPERATIONAL ELEMENTS INCLUDING: 1) TRIDYNE PRESSURANT, 2) DISTRIBUTED STORAGE AND CONTROL, 3) COLD GAS STORAGE / WARM GAS DELIVERY, 4) VARIABLE CASCADING RESIDUAL MANAGEMENT, AND 5) END-OF-BURN TANK PRESSURE DECAY. PUMP-FED LAUNCH VEHICLES WILL BENEFIT FROM OUR INNOVATIVE CONCEPT BUT THE MOST SIGNIFICANT BENEFITS WILL BE ACHIEVED IN COST-OPTIMIZED PRESSURE-FED SYSTEMS SUCH AS KT ENGINEERING S RADIALLY SEGMENTED LAUNCH VEHICLE (RSLV). WE PROPOSE AN 8-MONTH PHASE III PROGRAM TO DEVELOP AND PROVE KEY COMPONENTS OF THIS GROUND BREAKING APPROACH TO AFFORDABLE PRESSURE-FED PROPELLANT SYSTEMS. UNDER THE PROPOSED EFFORT WE WILL DEMONSTRATE FEASIBILITY AND MORE ACCURATELY QUANTIFY THE BENEFITS OF TRIDYNE PRESSURIZATION THROUGH DESIGN, FABRICATION, AND HIGH-FLOW, HIGH-PRESSURE TESTING OF A SINGLE BRANCH OF A REPRESENTATIVE TRIDYNE PRESSURIZATION SYSTEM INCLUDING A STORAGE BOTTLE, TUBING, CONTROL VALVE, INSTRUMENTATION, AND CATALYTIC REACTOR. THE PRODUCT OF THE EFFORT WILL BE ENGINEERING MODELS, TECHNICAL REPORTS, AND PRESENTATION MATERIALS FROM REVIEWS. WE PROPOSE A FIXED PRICE, MILESTONE BASED CONTRACT WITH AND EIGHT (8) MONTH PERIOD OF PERFORMANCE AND A TOTAL VALUE OF $99,792. | KT ENGINEERING CORPORATION | $99,792 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541330Engineering Services | B539SPECIAL STUDIES/ANALYSIS- AERONAUTICAL/SPACE | Aug 18, 2014 | Aug 18, 2014 | Jul 1, 2015 | ||
| KT ENGINEERING (KTE) IS PLEASED TO SUBMIT THIS PROPOSAL TO ADDRESS THE STATED NEED FOR "INNOVATIVE SOLUTIONS THAT WILL ALLOW SPACEPORT LAUNCH SERVICE PROVIDERS TO OPERATE IN AN EFFICIENT, LOW COST MANNER AND INCREASES CAPABILITIES ASSOCIATED WITH INTEGRATION, CHECKOUT, AND PREPARATIONS REQUIRED TO CONFIGURE AND READY SPACE SYSTEMS FOR LAUNCH." WE PROPOSE TO CONDUCT RESEARCH AND DEMONSTRATE FEASIBILITY OF A NOVEL LAUNCH VEHICLE PRESSURIZATION SYSTEM CONCEPT THAT WILL INCREASE PERFORMANCE AND RELIABILITY COMPARED WITH TRADITIONAL APPROACHES, REDUCE DEPENDENCE UPON HELIUM UP TO 50%, ENABLE THE USE OF LOW-COST COMMERCIAL OFF THE SHELF TECHNOLOGY, AND DEMONSTRATE THE AUTOMATED GROUND PROCESSING ASSOCIATED WITH THIS TECHNOLOGY. OUR INNOVATION IS BASED ON FIVE MAJOR TECHNOLOGY AND OPERATIONAL ELEMENTS INCLUDING: 1) TRIDYNE PRESSURANT, 2) DISTRIBUTED STORAGE AND CONTROL, 3) COLD GAS STORAGE / WARM GAS DELIVERY, 4) BANG-BANG PRESSURE CONTROL, AND 5) END-OF-BURN TANK PRESSURE DECAY. PUMP-FED LAUNCH VEHICLES WILL BENEFIT FROM OUR INNOVATIVE CONCEPT BUT THE MOST SIGNIFICANT BENEFITS ARE ACHIEVED IN COST-OPTIMIZED PRESSURE-FED SYSTEMS SUCH AS KT ENGINEERING'S RADIALLY SEGMENTED LAUNCH VEHICLE (RSLV). WE PROPOSE A SIX MONTH PHASE I PROGRAM TO REFINE THE DESIGNS OF THE CRITICAL GROUND AND AIRBORNE ELEMENTS OF THIS DISTRIBUTED PRESSURIZATION SYSTEM. WE INTEND TO DEMONSTRATE FEASIBILITY AND MORE ACCURATELY QUANTIFY THE BENEFITS OF OUR APPROACH THROUGH ANALYTICAL MODELING, PRELIMINARY DESIGN, AND HIGH-FLOW, HIGH-PRESSURE TESTING OF A PROTOTYPE TRIDYNE CATALYTIC REACTOR. THE PRODUCT OF THIS EFFORT WILL BE ENGINEERING ANALYSIS AND MODELS, PRESENTATION MATERIALS FROM MAJOR REVIEWS, A COMPREHENSIVE FINAL REPORT, AND OUR PHASE II PROPOSAL. UNDER PHASE II WE WILL PROPOSED TO DEMONSTRATE DESIGN AND OPERATION OF THE GROUND AND AIRBORNE ELEMENTS OF OUR PRESSURIZATION SYSTEM THROUGH PROTOTYPE HARDWARE FABRICATION AND TESTING IN THE NASA KSC LAUNCH EQUIPMENT TEST FACILITY (LETF). | KT ENGINEERING CORPORATION | $124,351 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCH | Feb 13, 2012 | Feb 13, 2012 | Aug 13, 2012 | ||
| THE CONTRACTOR SHALL PERFORM A RESEARCH AND DEVELOPMENT EFFORT TO DEMONSTRATE FEASIBILITY AND REDUCE TECHNICAL RISK ASSOCIATED WITH A TRANSPORTATION SYSTEM KNOWN AS THE RADIALLY SEGMENTED LAUNCH VEHICLE (RSLV). | KT ENGINEERING CORPORATION | $865,308 | DEFENSE ADVANCED RESEARCH PROJECTS AGENCY (DARPA) | DEFENSE ADVANCED RESEARCH PROJECTS AGENCY (DARPA) | — | 541712 | AD92 | Jun 24, 2011 | Jun 24, 2011 | Nov 24, 2012 | ||
| THIS PROPOSAL RESPONDS TO SUBTOPIC O2.02 "PROPULSION TECHNOLOGIES" AND THE STATED NEED TO DEVELOP COMPONENT TECHNOLOGIES THAT WILL LEAD TO FUTURE PROPULSION SYSTEMS THAT ARE RELIABLE AND HAVE ADEQUATE PERFORMANCE WITHOUT REQUIRING EXCESSIVE SPECIALIZED HANDLING EQUIPMENT AND PROCEDURES OR NEEDING TO PUSH MATERIALS AND DESIGNS TO THE LIMITS OF THEIR CAPABILITIES. WE PROPOSE THE DEVELOPMENT OF A LOW PART COUNT AND LOW ENERGY CATALYTICALLY INITIATED COMBUSTOR (CIC) THAT CAN SERVE AS A ROCKET ENGINE IGNITER AS WELL AS THE BASIS FOR A FAMILY OF LOW COST AND HIGHLY RELIABLE LAUNCH VEHICLE AND SATELLITE THRUSTERS. WE PROPOSE A 6-MONTH PHASE I PROGRAM TO 1) DEMONSTRATE RELIABLE IGNITION AND OPERATION OF OUR BASELINE CIC WITH HYDROGEN, METHANE, AND PROPANE FUELS, 2) DEMONSTRATE RELIABLE IGNITION AND OPERATION OF OUR BASELINE CIC UNDER COLD GAS INLET CONDITIONS, 3) DEMONSTRATE EXTENDED DURATION HOT FIRE TESTING AND DURABILITY OF OUR CIC DESIGN OVER MULTIPLE IGNITION CYCLES, AND 4) DEMONSTRATE RAPID PULSED OPERATION NECESSARY FOR A LAUNCH VEHICLE OR SPACE CRAFT THRUSTER APPLICATION. UNDER OUR PROPOSED PHASE I EFFORT, WE WILL ALSO CONDUCT A MARKET SURVEY OF POTENTIAL CUSTOMERS AND DEFINE A FLIGHT WEIGHT CIC WITH MAXIMUM COMMERCIAL UTILITY AS EITHER AN IGNITER OR SMALL THRUSTER. | KT ENGINEERING CORPORATION | $99,257 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCH | Feb 17, 2011 | Feb 18, 2011 | Sep 29, 2011 | ||
| SBIR PHASE III "RADIALLY SEGMENTED LAUNCH VEHICLE GROUND INTERFACE DEFINITION STUDY" | KT ENGINEERING CORPORATION | $0 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541330Engineering Services | R425SUPPORT- PROFESSIONAL: ENGINEERING/TECHNICAL | Aug 31, 2010 | Aug 31, 2010 | Sep 30, 2010 | ||
| PHASE III SBIR: RADIALLY SEGMENTED LAUNCH VEHICLE OXYGEN / METHANE TECHNOLOGY MATURATION PROGRAM THE CONTRACTOR'S EFFORT DESCRIBED IN THE PROPOSAL INVOLVES FOUR MAJOR TASKS. THESE TASKS ARE: 1. CATALYTICALLY INITIATED COMBUSTOR DEVELOPMENT. THE CATALYTICALLY INITIATED COMBUSTOR (CIC) CONCEPT WAS CONCEIVED BY KT ENGINEERING UNDER AND INDEPENDENT RESEARCH AND DEVELOPMENT (IR&D) PROGRAM AND REFINED UNDER SBIR PHASE II CONTRACT F29601-02-C-0010 WITH AFRL AND NASA SBIR PHASE III CONTRACT NNM09AA33C. THE PROPOSED TASK I ACTIVITIES, WITHIN THIS NASA SBIR PHASE III PROGRAM, WILL CONTINUE TO RETIRE TECHNICAL RISK ASSOCIATED WITH CONCEPT AND RAISE THE NASA TRL. THE EFFORT WILL REFINE THE CIC DESIGN TO ADDITIONAL SEA LEVEL TESTING USING GASEOUS PROPELLANTS. THIS ADDITIONAL TESTING IS REQUIRED TO DEMONSTRATE CIC OPERATION UNDER HIGH FLOW, HIGH CHAMBER PRESSURE CONDITIONS INCLUDING THE USE OF ABLATIVE CHAMBERS IN CONJUNCTION WITH HIGHER MIXTURE RATIOS TO REDUCE RISK ASSOCIATED WITH THE USE OF THE CIC IN A REACTION CONTROL SYSTEM APPLICATION. 2. HIGHLY RELIABLE, ROCKET ENGINE INJECTOR FABRICATION. KT ENGINEERING INVESTIGATED THE USE OF INVESTMENT CASTING TO PRODUCE A NEAR-NET INJECTOR BODY FOR A LO2/LCH4 ROCKET ENGINE UNDER SBIR PHASE II CONTRACT F29601-02-C-0010 WITH AFRL. THE FOCUS OF THIS EFFORT WAS TO SIGNIFICANTLY LOWER RECURRING COST BY REDUCING MACHINING TIME AND RAW MATERIAL REQUIREMENTS. HOWEVER, THE AFRL EFFORT ALSO IDENTIFIED THE NEED FOR A STRUCTURED ENGINEERING INVESTIGATION TO IDENTIFY THE OPTIMAL METHODS FOR PRODUCING THE DISPOSABLE MOLDS, REMOVING THE CERAMIC CRES USED TO CREATE THE INTERNAL RING MANIFOLDS, AND NON-DESTRUCTIVE EVALUATION OF THE CONTRACT NNM09AA33C THROUGH THE DEVELOPMENT OF DESIGNS, TOOLS, MANUFACTURING PROCESSES, AND THE CASTING OF SIMPLIFIED INJECTOR PROCESS PATHFINDERS. THE RESULTS FROM THE NASA SBIR PHASE III CONTINUE TO INDICATE THAT AN INTEGRAL-FACE, CAST INJECTOR IS FEASIBLE. THE PROPOSED TASK 2 ACTIVITY IS THE NEXT LOGICAL STEP TO REDUCE RISK ASSOCIATED WITH THIS TECHNOLOGY BY DEMONSTRATING ITS UTILITY ON A MORE COMPLEX INJECTOR PROTOTYPE THAT MORE CLOSELY REPRESENTS THE SIZE, SHAPE, AND GEOMETRY OF A FLIGHT WEIGHT INJECTOR. 3. PRESSURIZATION SYSTEM DEMONSTRATION. THE RSVL USES AN INNOVATIVE, DISTRIBUTED PRESSURIZATION SYSTEM TO PROVIDE INERT GAS FOR PURGES, VALVE ACTUATION, AND TANK PRESSURIZATION DURING FLIGHT. THE APPROACH PROMISES TO BE MORE RELIABLE, LESS COSTLY, AND HIGHER PERFORMING THAN A CONVENTIONAL BLOW-DOWN PRESSURIZATION SYSTEM FOR A PRESSURE-FED VEHICLE. UNDER THROUGH RIGOROUS ENGINEERING MODELING AND LIMITED BENCH-TOP TESTING. THE NEXT LOGICAL STEP, TASK 3 OF THIS PROPOSAL, IS TO INCREASE THE RRL AND VALIDATE THE APPROACH THROUGH COMPONENT AND SYSTEM LEVEL DEVELOPMENT AT PRESSURES AND FLOW RATES CONSISTENT WITH THE REQUIREMENTS FOR THE RSLV. 4. ENGINE MODULE TESTING. EXPERIENCE HAS SHOWN THAT PROPULSION SYSTEMS COMPONENTS MUST ULTIMATELY BE INTEGRATED INTO A COMPLETE ENGINE SYSTEM AND RIGOROUSLY TESTED UNDER ALL ANTICIPATED SERVICE ENVIRONMENTS AND CONDITIONS. KT ENGINEERING HAS DEVELOPED AND DEMONSTRATED A NUMBER OF COMPONENT TECHNOLOGIES APPLICABLE TO THE RSLV PROPULSION SYSTEM. THE NEXT CRITICAL STEP IS TO DEMONSTRATE THESE TECHNOLOGIES INTEGRATED INTO AN OPERATIONAL ENGINE MODULE. KT ENGINEERING DEVELOPED THE DESIGN FOR A FLIGHT WEIGHT RSLV ENGINE MODULE UNDER SBIR PHASE III CONTRACT FA9453-08-C-0171 WITH AFRL. A PROTOTYPE ENGINE MODULE WAS PARTIALLY FABRICATED, INTEGRATED, AND TESTED BEFORE THE CONTRACT ENDED. UNDER TASK 4 OF THIS PROPOSAL, KT ENGINEERING WILL COMPLETE THE ENGINE MODULE, INTEGRATE THE UPDATED CATALYTIC IGNITER AND RCS THRUSTER DESIGNS, UPGRADE THE INJECTOR, PRESSURIZATION AND FEED SYSTEMS BASED ON LESSONS LEARNED, AND PERFORM TESTING OF THE ENGINE ON A MODULAR TEST. | KT ENGINEERING CORPORATION | $1,000,000 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541330Engineering Services | AD24 | May 19, 2010 | May 19, 2010 | Feb 22, 2012 | ||
| PHASE III SBIR: RADIALLY SEGMENTED LAUNCH VEHICLE OXYGEN / METHANE TECHNOLOGY MATURATION PROGRAM | KT ENGINEERING CORPORATION | $0 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541330Engineering Services | AD24 | Sep 15, 2009 | Sep 14, 2009 | Feb 28, 2010 | ||
| SBIR III | KT ENGINEERING CORPORATION | $5,131,173 | DEPT OF THE AIR FORCE | DEPT OF THE AIR FORCE | — | 541712 | AC25NATIONAL DEFENSE R&D SVCS; ATOMIC ENERGY DEFENSE ACTIVITIES; R&D FACILITIES & MAJ EQUIP | Oct 29, 2007 | Oct 29, 2007 | Apr 1, 2009 | ||
| FABRICATION OF COLD FLOW NOZZLE TIC4 AND ST2 TO SUPPORT THE J2X ENGINE PROGRAM | KT ENGINEERING CORPORATION | $77,388 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | 332313Plate Work Manufacturing | 3695MISCELLANEOUS SPECIAL INDUSTRY MACHINERY | Jul 6, 2007 | Jul 6, 2007 | Mar 18, 2008 | ||
| J2X COLD FLOW SIDE LOAD NOZZLE DESIGN AND FABRICATION | KT ENGINEERING CORPORATION | $29,747 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | 541710 | AJ44 | Apr 3, 2007 | Apr 3, 2007 | Nov 16, 2007 | ||
| CEV PROPULSION ADVANCED DEVELOPMENT 7500 LBF (VACUUM) MAIN ENGINE | KT ENGINEERING CORPORATION | $0 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | 541710 | AR13SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; EXPERIMENTAL DEVELOPMENT | May 4, 2006 | Apr 27, 2006 | Jan 29, 2010 | ||
| 4200117603 NOZZLE TEST ARTICLE | KT ENGINEERING CORPORATION | $12,737 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | — | — | Jul 1, 2005 | Jul 1, 2005 | Jan 2, 2006 | ||
| SEGMENTED LAUNCH VEHICLE MFG DEV & DEMO PROGRAM (DARPA BAA) | KT ENGINEERING CORPORATION | $9,146,792 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 927110Space Research and Technology | 1820 | Aug 6, 2004 | Aug 6, 2004 | Apr 30, 2009 | ||
| 4200055908 PRELIMINARY RSLV DESIGN STUDIES | KT ENGINEERING CORPORATION | $99,418 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | 541710 | AC31NATIONAL DEFENSE R&D SERVICES; DEFENSE-RELATED ACTIVITIES; BASIC RESEARCH | May 19, 2004 | May 26, 2004 | Aug 19, 2004 | ||
| 4200048915 UPGRADE AND ENHANCEMENT OF OPERATION COST MODEL IN 2004 | KT ENGINEERING CORPORATION | $259,116 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | 541710 | AR46 | Mar 31, 2004 | Apr 1, 2004 | Sep 30, 2006 | ||
| 4200044631 SBIR PHASE 1 ALTITUDE COMPENSATING NOZZLE DESIGN TOOL | KT ENGINEERING CORPORATION | $69,809 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | 541710 | AR91 | Jan 16, 2004 | Jan 16, 2004 | Jul 19, 2004 | ||
| SBIR 2003 PHASE I AWARD. | KT ENGINEERING CORPORATION | $69,920 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | 541330Engineering Services | AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCH | Jan 16, 2004 | Jan 16, 2004 | Jul 15, 2004 | ||
| — | KT ENGINEERING CORPORATION | $0 | DEFENSE ADVANCED RESEARCH PROJECTS AGENCY (DARPA) | DEFENSE ADVANCED RESEARCH PROJECTS AGENCY (DARPA) | — | 541710 | AD93 | Nov 14, 2003 | Nov 14, 2003 | — | ||
| UPDATE/UPGRADE CONCEPTUAL OPS MANPOWER EST TOOL & OPS COST MODEL | KT ENGINEERING CORPORATION | $218,673 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | 541710 | R425SUPPORT- PROFESSIONAL: ENGINEERING/TECHNICAL | Aug 22, 2002 | Aug 22, 2002 | Mar 31, 2004 | ||
| 200206!000217!5700!GS05 !DET 8 AFRL/PK (SUPPORTS VS) !F2960102C0010 !A!N! !N! !20020320!20030623!127963515!127963515!127963515!N!KT ENGINEERING CORPORATION !4835 UNIVERSITY SQUARE !HUNTSVILLE !AL!35816!09976!089!01!BROWNSBORO !MADISON !ALABAMA !+000001037885!N!N!000001037885!AC26!RDTE/MISSILE AND SPACE SYSTEMS-MGMT SUPPORT !A2 !MISSILE AND SPACE SYSTEMS !3CAA!BALLISTIC MISSILE DEFENSE SYS !541710!E! !3! ! ! ! ! !99990909!B! ! !B! !A!N!U!2!001!K! !Z!Y!Z! ! !N!B!N!N! ! !A! !B!A!000!C!B!N! ! ! ! ! ! !0001! | KT ENGINEERING CORPORATION | $0 | DEPT OF THE AIR FORCE | DEPT OF THE AIR FORCE | — | 541710 | AC25NATIONAL DEFENSE R&D SVCS; ATOMIC ENERGY DEFENSE ACTIVITIES; R&D FACILITIES & MAJ EQUIP | Mar 20, 2002 | Mar 20, 2002 | Sep 28, 2007 | ||
| 200008!5700!000211!GS05 !DET 8 AFRL/PK (SUPPORTS VS) !F2960100C0032 !A!*!* !20000501!20010101!127963515!127963515!127963515!N!1PKT4!KT ENGINEERING L.L.C !600 SUNBURST CIRCLE !BROWNSBORO !AL!35741!09976!089!01!BROWNSBORO !MADISON !ALABAMA !0001!+000000039987!N!N!000000000000!AC26!RDTE/MISSILE AND SPACE SYSTEMS-MGMT SUPPORT !A2 !MISSILE AND SPACE SYSTEMS !3000!NOT DISCERNABLE OR CLASSIFIED !8731!3!*!*!*!B!A!*!A !N!J!2!001!K!* !Z!N!Z!* !* !N!B!N!A!*!B!A!A!A!* !*!N!B!B!N!*!*!*!*!*! | KT ENGINEERING CORPORATION | $0 | DEPT OF THE AIR FORCE | — | — | — | AC26 | May 1, 2000 | May 1, 2000 | — | ||
| — | KT ENGINEERING CORPORATION | $0 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | 541710 | B599SPECIAL STUDIES/ANALYSIS- OTHER | Apr 15, 2000 | Apr 15, 2000 | Dec 15, 2000 |