Discover Opportunities months before the RFP drops
Learn more →Retrieving contract details... Hang tight!
See what competitors charge and their contract structure
Spot renewal opportunities 6-12 months before expiration
Analyze buyer's purchasing history and vendor preferences
Track expiration dates across all your target accounts
Reach decision-makers before renewal with competitive intel
Our customers win 3x more contract renewals and replacements
Verified decision-maker contacts
Winning vendor information
Budget & renewal data
Clean & enrich your CRM automatically
Track contract spending & renewal dates
Analyze historical pricing trends
Identify upcoming opportunities
Get complete source documentation & analysis
NIH NCI
This contract includes 1 purchase order from Feb 1, 2022 to Feb 1, 2022
| Buyer | Vendor | Issued Date | Quantity |
|---|---|---|---|
| NIH NCI | Leidos Biomedical Research, Inc. | Feb 1, 2022 | 1 |
Full Purchase Intelligence Available
Get complete pricing, descriptions, and financial details for all 1 purchase orders
Unlock Full Details →See what competitors charge and their contract structure
Spot renewal opportunities 6-12 months before expiration
Analyze buyer's purchasing history and vendor preferences
Track expiration dates across all your target accounts
Reach decision-makers before renewal with competitive intel
Our customers win 3x more contract renewals and replacements
No public files available for this contract.
Contract documentation may be available through official government sources or agency portals. Starbridge can help you track down and retrieve these files.
Department of Defense
ENGINEERING, MANUFACTURING , DEVELOPMENT, AND PRODUCTION OF A COMMON BOMBER ARMAMENT TESTER.
Effective Date
Sep 28, 2017
Expires
Effective: Sep 28, 2017
Department of Defense
Expires:
ENGINEERING, MANUFACTURING , DEVELOPMENT, AND PRODUCTION OF A COMMON BOMBER ARMAMENT TESTER.
ActiveNaval Sea Systems Command Headquarters
DESIGN, DEVELOPMENT, TESTING, SYSTEM SUPPORT, AND PRODUCTION OF SUBMARINE PHOTONICS MASTS
Effective Date
Jul 2, 2020
Expires
Naval Sea Systems Command Headquarters
Expires:
DESIGN, DEVELOPMENT, TESTING, SYSTEM SUPPORT, AND PRODUCTION OF SUBMARINE PHOTONICS MASTS
ActiveNASA Marshall Space Flight Center
PROVIDE DEVELOPMENTAL HARDWARE AND TEST ARTICLES, AND MANUFACTURE AND ASSEMBLE ARES I UPPER STAGES. THE UPPER STAGE (US) ELEMENT IS AN INTEGRAL PART OF THE ARES I LAUNCH VEHICLE AND PROVIDES THE SECOND STAGE OF FLIGHT. THE US ELEMENT IS RESPONSIBLE FOR THE ROLL CONTROL DURING THE FIRST STAGE BURN AND SEPARATION; AND WILL PROVIDE THE GUIDANCE AND NAVIGATION, COMMAND AND DATA HANDLING, AND OTHER AVIONICS FUNCTIONS FOR THE ARES I DURING ALL PHASES OF THE ASCENT FLIGHT. THE US ELEMENT IS A NEW DESIGN THAT EMPHASIZES SAFETY, OPERABILITY, AND MINIMUM LIFE CYCLE COST. THE OVERALL DESIGN, DEVELOPMENT, TEST AND EVALUATION (DDT&E), PRODUCTION, AND SUSTAINING ENGINEERING EFFORTS INCLUDE ACTIVITIES PERFORMED BY THREE ORGANIZATIONS; THE NASA DESIGN TEAM (NDT), THE UPPER STAGE PRODUCTION CONTRACTOR (USPC) AND THE INSTRUMENT UNIT PRODUCTION CONTRACTOR (IUPC). FOR CLARITY, THE USPC WILL BE REFERRED TO AS THE CONTRACTOR THROUGHOUT THIS DOCUMENT. NASA IS RESPONSIBLE FOR THE INTEGRATION OF THE PRIMARY ELEMENTS OF THE ARES I LAUNCH VEHICLE INCLUDING: THE FIRST STAGE, US INCLUDING INSTRUMENT UNIT (IU), AND US ENGINE; AND WILL ALSO INTEGRATE THE ARES I LAUNCH VEHICLE AT THE LAUNCH SITE. NASA IS RESPONSIBLE FOR THE DDT&E, INCLUDING TECHNICAL AND PROGRAMMATIC INTEGRATION OF THE US SUBSYSTEMS AND GOVERNMENT-FURNISHED PROPERTY. NASA WILL LEAD THE EFFORT TO DEVELOP THE REQUIREMENTS AND SPECIFICATIONS OF THE US ELEMENT, THE DEVELOPMENT PLAN AND TESTING REQUIREMENTS, AND ALL DESIGN DOCUMENTATION, INITIAL MANUFACTURING AND ASSEMBLY PROCESS PLANNING, LOGISTICS PLANNING, AND OPERATIONS SUPPORT PLANNING. DEVELOPMENT, QUALIFICATION, AND ACCEPTANCE TESTING WILL BE CONDUCTED BY NASA AND THE CONTRACTOR TO SATISFY REQUIREMENTS AND FOR RISK MITIGATION. NASA IS RESPONSIBLE FOR THE OVERALL UPPER STAGE VERIFICATION AND VALIDATION PROCESS AND WILL REQUIRE SUPPORT FROM THE CONTRACTOR. THE CONTRACTOR IS RESPONSIBLE FOR THE MANUFACTURE AND ASSEMBLY OF THE UPPER STAGE TEST FLIGHT AND OPERATIONAL UPPER STAGE UNITS INCLUDING THE INSTALLATION OF UPPER STAGE INSTRUMENT UNIT, THE GOVERNMENT-FURNISHED US ENGINE, BOOSTER SEPARATION MOTORS, AND OTHER GOVERNMENT-FURNISHED PROPERTY. A DESCRIPTION OF THE NASA MANAGED AND PERFORMED EFFORTS IS CONTAINED IN THE US WORK PACKAGES AND WILL BE MADE AVAILABLE TO THE CONTRACTOR TO ENSURE THEIR UNDERSTANDING OF THE ROLES AND RESPONSIBILITIES OF THE NDT, IUPC, AND CONTRACTOR DURING THE DESIGN, DEVELOPMENT, AND OPERATION OF THE US ELEMENT. THE US CONCEPTUAL DESIGN DESCRIBED IN THE USO-CLV-SE-25704 US DESIGN DEFINITION DOCUMENT (DDD) IS THE BASELINE DESIGN FOR THIS CONTRACT. THE CONTRACTORS EARLY ROLE WILL BE TO PROVIDE PRODUCIBILITY ENGINEERING SUPPORT TO NASA VIA THE ESTABLISHED US OFFICE STRUCTURE AND TO PROVIDE INPUTS INTO THE FINAL DESIGN CONFIGURATION, SPECIFICATIONS, AND STANDARDS. NASA WILL TRANSITION THE MANUFACTURING AND ASSEMBLY, LOGISTICS SUPPORT INFRASTRUCTURE, CONFIGURATION MANAGEMENT, AND THE SUSTAINING ENGINEERING FUNCTIONS TO THE CONTRACTOR AT THE KEY POINTS DURING THE DEVELOPMENT AND IMPLEMENTATION OF THE PROGRAM CURRENTLY PLANNED TO OCCUR NO LATER THAN 90 DAYS AFTER THE COMPLETION OF THE FOLLOWING MAJOR MILESTONES: MANUFACTURING AND ASSEMBLY US PRELIMINARY DESIGN REVIEW (PDR) LOGISTICS SUPPORT INFRASTRUCTURE US PDR CONFIGURATION MANAGEMENT US CRITICAL DESIGN REVIEW CDR) SUSTAINING ENGINEERING US DESIGN CERTIFICATION REVIEW (DCR) AFTER THE COMPLETION OF AN ORDERLY TRANSITION OF ROLES AND RESPONSIBILITIES TO THE CONTRACTOR, NASA WILL ASSUME AN INSIGHT ROLE INTO THE CONTRACTORS PRODUCTION, SUSTAINING ENGINEERING, AND OPERATIONS SUPPORT OF THE ARES I US TEST PROGRAM AND FLIGHT HARDWARE. AFTER DCR, THE CONTRACTOR WILL BE RESPONSIBLE FOR SUSTAINING ENGINEERING PER SOW SECTION 4.7, AS NECESSARY TO MAINTAIN AND SUPPORT THE US CONFIGURATION AND FOR PRODUCTION AND OPERATIONS SUPPORT.
Effective Date
Sep 1, 2007
Expires
Effective: Sep 1, 2007
NASA Marshall Space Flight Center
Expires:
PROVIDE DEVELOPMENTAL HARDWARE AND TEST ARTICLES, AND MANUFACTURE AND ASSEMBLE ARES I UPPER STAGES. THE UPPER STAGE (US) ELEMENT IS AN INTEGRAL PART OF THE ARES I LAUNCH VEHICLE AND PROVIDES THE SECOND STAGE OF FLIGHT. THE US ELEMENT IS RESPONSIBLE FOR THE ROLL CONTROL DURING THE FIRST STAGE BURN AND SEPARATION; AND WILL PROVIDE THE GUIDANCE AND NAVIGATION, COMMAND AND DATA HANDLING, AND OTHER AVIONICS FUNCTIONS FOR THE ARES I DURING ALL PHASES OF THE ASCENT FLIGHT. THE US ELEMENT IS A NEW DESIGN THAT EMPHASIZES SAFETY, OPERABILITY, AND MINIMUM LIFE CYCLE COST. THE OVERALL DESIGN, DEVELOPMENT, TEST AND EVALUATION (DDT&E), PRODUCTION, AND SUSTAINING ENGINEERING EFFORTS INCLUDE ACTIVITIES PERFORMED BY THREE ORGANIZATIONS; THE NASA DESIGN TEAM (NDT), THE UPPER STAGE PRODUCTION CONTRACTOR (USPC) AND THE INSTRUMENT UNIT PRODUCTION CONTRACTOR (IUPC). FOR CLARITY, THE USPC WILL BE REFERRED TO AS THE CONTRACTOR THROUGHOUT THIS DOCUMENT. NASA IS RESPONSIBLE FOR THE INTEGRATION OF THE PRIMARY ELEMENTS OF THE ARES I LAUNCH VEHICLE INCLUDING: THE FIRST STAGE, US INCLUDING INSTRUMENT UNIT (IU), AND US ENGINE; AND WILL ALSO INTEGRATE THE ARES I LAUNCH VEHICLE AT THE LAUNCH SITE. NASA IS RESPONSIBLE FOR THE DDT&E, INCLUDING TECHNICAL AND PROGRAMMATIC INTEGRATION OF THE US SUBSYSTEMS AND GOVERNMENT-FURNISHED PROPERTY. NASA WILL LEAD THE EFFORT TO DEVELOP THE REQUIREMENTS AND SPECIFICATIONS OF THE US ELEMENT, THE DEVELOPMENT PLAN AND TESTING REQUIREMENTS, AND ALL DESIGN DOCUMENTATION, INITIAL MANUFACTURING AND ASSEMBLY PROCESS PLANNING, LOGISTICS PLANNING, AND OPERATIONS SUPPORT PLANNING. DEVELOPMENT, QUALIFICATION, AND ACCEPTANCE TESTING WILL BE CONDUCTED BY NASA AND THE CONTRACTOR TO SATISFY REQUIREMENTS AND FOR RISK MITIGATION. NASA IS RESPONSIBLE FOR THE OVERALL UPPER STAGE VERIFICATION AND VALIDATION PROCESS AND WILL REQUIRE SUPPORT FROM THE CONTRACTOR. THE CONTRACTOR IS RESPONSIBLE FOR THE MANUFACTURE AND ASSEMBLY OF THE UPPER STAGE TEST FLIGHT AND OPERATIONAL UPPER STAGE UNITS INCLUDING THE INSTALLATION OF UPPER STAGE INSTRUMENT UNIT, THE GOVERNMENT-FURNISHED US ENGINE, BOOSTER SEPARATION MOTORS, AND OTHER GOVERNMENT-FURNISHED PROPERTY. A DESCRIPTION OF THE NASA MANAGED AND PERFORMED EFFORTS IS CONTAINED IN THE US WORK PACKAGES AND WILL BE MADE AVAILABLE TO THE CONTRACTOR TO ENSURE THEIR UNDERSTANDING OF THE ROLES AND RESPONSIBILITIES OF THE NDT, IUPC, AND CONTRACTOR DURING THE DESIGN, DEVELOPMENT, AND OPERATION OF THE US ELEMENT. THE US CONCEPTUAL DESIGN DESCRIBED IN THE USO-CLV-SE-25704 US DESIGN DEFINITION DOCUMENT (DDD) IS THE BASELINE DESIGN FOR THIS CONTRACT. THE CONTRACTORS EARLY ROLE WILL BE TO PROVIDE PRODUCIBILITY ENGINEERING SUPPORT TO NASA VIA THE ESTABLISHED US OFFICE STRUCTURE AND TO PROVIDE INPUTS INTO THE FINAL DESIGN CONFIGURATION, SPECIFICATIONS, AND STANDARDS. NASA WILL TRANSITION THE MANUFACTURING AND ASSEMBLY, LOGISTICS SUPPORT INFRASTRUCTURE, CONFIGURATION MANAGEMENT, AND THE SUSTAINING ENGINEERING FUNCTIONS TO THE CONTRACTOR AT THE KEY POINTS DURING THE DEVELOPMENT AND IMPLEMENTATION OF THE PROGRAM CURRENTLY PLANNED TO OCCUR NO LATER THAN 90 DAYS AFTER THE COMPLETION OF THE FOLLOWING MAJOR MILESTONES: MANUFACTURING AND ASSEMBLY US PRELIMINARY DESIGN REVIEW (PDR) LOGISTICS SUPPORT INFRASTRUCTURE US PDR CONFIGURATION MANAGEMENT US CRITICAL DESIGN REVIEW CDR) SUSTAINING ENGINEERING US DESIGN CERTIFICATION REVIEW (DCR) AFTER THE COMPLETION OF AN ORDERLY TRANSITION OF ROLES AND RESPONSIBILITIES TO THE CONTRACTOR, NASA WILL ASSUME AN INSIGHT ROLE INTO THE CONTRACTORS PRODUCTION, SUSTAINING ENGINEERING, AND OPERATIONS SUPPORT OF THE ARES I US TEST PROGRAM AND FLIGHT HARDWARE. AFTER DCR, THE CONTRACTOR WILL BE RESPONSIBLE FOR SUSTAINING ENGINEERING PER SOW SECTION 4.7, AS NECESSARY TO MAINTAIN AND SUPPORT THE US CONFIGURATION AND FOR PRODUCTION AND OPERATIONS SUPPORT.
ActiveSee who's winning contracts, track spending trends, and identify your best opportunities before your competition.
Schedule Your Demo →Verified decision-maker contacts
Winning vendor information
Budget & renewal data
Clean & enrich your CRM automatically
Track contract spending & renewal dates
Analyze historical pricing trends
Identify upcoming opportunities
Get complete source documentation & analysis
NASA Marshall Space Flight Center
FIRST DDT AND E, ARES I-X, AND FLIGHT TESTS. FIRST STAGE WILL BE A FIVE SEGMENT, SOLID ROCKET BOOSTER DERIVED FROM THE SPACE SHUTTLE PROGRAM (SSP) SOLID ROCKET BOOSTER (SRB)/REUSABLE SOLID ROCKET MOTOR (RSRM). THE CONTRACTOR SHALL FURNISH THE NECESSARY MANAGEMENT, ENGINEERING, LABOR, FACILITIES, TOOLS, EQUIPMENT, AND MATERIALS REQUIRED FOR FIRST STAGE DEVELOPMENT, QUALIFICATION, CERTIFICATION AND ACCEPTANCE PROGRAM. ACTIVITIES INCLUDE: REDESIGN AND TESTING OF THE MOTOR TO INCORPORATE THE FIFTH SEGMENT AND PRODUCTION OF FIVE FULL SCALE GROUND STATIC TEST MOTORS: TWO DEVELOPMENT MOTORS (DMS)-AND THREE QUALIFICATION MOTORS (QMS); STRUCTURAL TEST ARTICLE (STA), GROUND VIBRATION TEST MOTORS (GVTMS) AND OTHER DEVELOPMENT TESTING; REDESIGN OF THE AVIONICS, DECELERATION, SEPARATION, AND FLIGHT TERMINATION SYSTEM (FTS) SUBSYSTEMS; ARES I-X: SIMULATED ARES I OUTER MOLD LINE/MASS PROPERTIES USING MODIFIED SRB/RSRM; AND THREE FLIGHT TEST VEHICLES. TAS::80 0124::TAS
Effective Date
Apr 17, 2006
Expires
Effective: Apr 17, 2006
NASA Marshall Space Flight Center
Expires:
FIRST DDT AND E, ARES I-X, AND FLIGHT TESTS. FIRST STAGE WILL BE A FIVE SEGMENT, SOLID ROCKET BOOSTER DERIVED FROM THE SPACE SHUTTLE PROGRAM (SSP) SOLID ROCKET BOOSTER (SRB)/REUSABLE SOLID ROCKET MOTOR (RSRM). THE CONTRACTOR SHALL FURNISH THE NECESSARY MANAGEMENT, ENGINEERING, LABOR, FACILITIES, TOOLS, EQUIPMENT, AND MATERIALS REQUIRED FOR FIRST STAGE DEVELOPMENT, QUALIFICATION, CERTIFICATION AND ACCEPTANCE PROGRAM. ACTIVITIES INCLUDE: REDESIGN AND TESTING OF THE MOTOR TO INCORPORATE THE FIFTH SEGMENT AND PRODUCTION OF FIVE FULL SCALE GROUND STATIC TEST MOTORS: TWO DEVELOPMENT MOTORS (DMS)-AND THREE QUALIFICATION MOTORS (QMS); STRUCTURAL TEST ARTICLE (STA), GROUND VIBRATION TEST MOTORS (GVTMS) AND OTHER DEVELOPMENT TESTING; REDESIGN OF THE AVIONICS, DECELERATION, SEPARATION, AND FLIGHT TERMINATION SYSTEM (FTS) SUBSYSTEMS; ARES I-X: SIMULATED ARES I OUTER MOLD LINE/MASS PROPERTIES USING MODIFIED SRB/RSRM; AND THREE FLIGHT TEST VEHICLES. TAS::80 0124::TAS
Active