Office of the Administrator Awarded Contracts - Systems Engineering | Federal Compass

Office of the Administrator Awarded Contracts - Systems Engineering

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80TECH22PA016 - ITPOD AWARD, NETSCANNER PRESSURE SYSTEM, GLENN RESEARCH CENTER,(GRC) NASA.
Purchase Order - 541519 Other Computer Related Services
Contractor
MEASUREMENT SPECIALTIES, INC. (MEASUREMENT SPECIALTIES INC)
Contracting Agency/Office
National Aeronautics and Space Administration»Office of the Administrator»NASA Office of the Chief Information Officer»Information Technology Procurement Office
Effective date
09/28/2022
Obligated Amount
$394.6k
80TECH22PA009 - ITPOD AWARD, SCRAMJET TEST OPTIMUS SYSTEM FOR SCANNING FOR LARC, NASA.
Purchase Order - 541519 Other Computer Related Services
Contractor
MEASUREMENT SPECIALTIES, INC. (MEASUREMENT SPECIALTIES INC)
Contracting Agency/Office
National Aeronautics and Space Administration»Office of the Administrator»NASA Office of the Chief Information Officer»Information Technology Procurement Office
Effective date
09/22/2022
Obligated Amount
$242.9k
80TECH22PA006 - RTI ENGINEERING SUPPORT SERVICES CONTRACT
Purchase Order - 541511 Custom Computer Programming Services
Contractor
REAL-TIME INNOVATIONS, INC. (REAL-TIME INNOVATIONS INC)
Contracting Agency/Office
National Aeronautics and Space Administration»Office of the Administrator»NASA Office of the Chief Information Officer»Information Technology Procurement Office
Effective date
09/01/2022
Obligated Amount
$1.7M
80HQTR22DA003 - AERONAUTICS AND SPACE PROGRAMS AND POLICIES STUDIES
IDC - 541990 All Other Professional, Scientific, and Technical Services
Contractor
National Academy of Sciences (NATIONAL ACADEMY OF SCIENCES)
Contracting Agency/Office
National Aeronautics and Space Administration»Office of the Administrator
Effective date
02/16/2022
Obligated Amount
$3.7M
80HQTR19D0032 - ENSURING THAT VISITORS HAVE A MEANINGFUL, SATISFYING AND SAFE EXPERIENCE EXPLORING THE MANY DIMENSIONS OF NASA GODDARD BY PROMOTING AND INSPIRING FURTHER ENGAGEMENT IN NASA SCIENCES, TECHNOLOGY AND ENGINEERING.
IDC - 611710 Educational Support Services
Contractor
Alexton Incorporated (ALEXTON INCORPORATED)
Contracting Agency/Office
National Aeronautics and Space Administration»Office of the Administrator
Effective date
08/29/2019
Obligated Amount
$3.6M
80HQTR19C0018 - ISRU-DERIVED WATER PURIFICATION AND HYDROGEN OXYGEN PRODUCTION (IHOP) COMPONENT DEVELOPMENT
Definitive Contract - 541715 Research and Development in the Physical, Engineering, and Life Sciences
Contractor
Paragon Space Development Corporation (PARAGON SPACE DEVELOPMENT CORPORATION)
Contracting Agency/Office
National Aeronautics and Space Administration»Office of the Administrator
Effective date
05/06/2019
Obligated Amount
$1.5M
80HQTR17C0009 - NASA BAA/NRA AWARD. PROPOSAL TITLE "NEXT SPACE TECHNOLOGIES FOR EXPLORATION PARTNERSHIP - NEXTSTEP-2. THE NEXTSTEP-2 STUDY CONDUCTED BY SNC WILL EVALUATE MISSION ARCHITECTURE, SYSTEM INTERFACES, AND SUBSYSTEM COMPONENT DESIGN TO MEET THE OBJECTIVES OF THE THREE OPERATIONAL PHASES OUTLINED BY NASA. NASA'S HEOMD/AES DIVISION SELECTED THE SIERRA NEVADA CORPORATION PROPOSAL IN RESPONSE TO THE NEXT SPACE TECHNOLOGIES FOR EXPLORATION PARTNERSHIPS -2 (NEXTSTEP-2) BAA SOLICITATION IN THE AREA OF HABITATION SYSTEMS. THIS CONTRACT EFFORT WILL FOCUS ON REFINING ARCHITECTURES AND CONCEPTS OF OPERATION AND DEVELOPING A FULL SIZE GROUND BASED DEEP SPACE HABITATION PROTOTYPE UNIT FOR INITIAL HABITATION CAPABILITIES IN CISLUNAR SPACE WITH EXTENSIBILITY FOR IN-SPACE TRANSIT HABITATION. THIS CONTRACT WILL ALSO DEVELOP PLANS AND ESTIMATES FOR FURTHER ENGINEERING AND FLIGHT UNIT DEVELOPMENT AND PARTICIPATION IN A NASA-LED STANDARDS AND COMMON INTERFACES WORKING GROUP. KEY COMPONENTS AND TECHNOLOGIES WILL BE IDENTIFIED DURING THE STUDY PHASE. AS PART OF OPTION 1 SNC WILL DEVELOP A FULL-SCALE PROTOTYPE TO FURTHER MATURE THE DESIGN AND REDUCE RISK. TECHNOLOGIES AND SUBSYSTEMS WITH COMMERCIAL SPACE APPLICATIONS WILL BE IDENTIFIED BY SNC FOR USE IN EXPANDING SNC'S COMMERCIAL SPACE GOALS. ADDITIONALLY, THE TOTAL PROGRAM COSTS FOR EXECUTION THROUGH PHASE 2 WILL BE CONTINUALLY REFINED THROUGHOUT THE STUDY, AND CULMINATE IN A PROPOSAL FOR A FOLLOW-ON CONTRACT. THE PROPOSED SYSTEM ALLOWS FOR FLEXIBLE MATING OPTIONS TO CONNECT AND ACCOMMODATE A VARIETY OF ELEMENTS, INCLUDING DIFFERENT HABITAT ELEMENTS AND A DOCKING DESTINATION FOR NATIONAL AERONAUTICS AND SPACE ADMINISTRATION'S (NASA) ORION SPACECRAFT.
Definitive Contract - 541712 Research and Development in the Physical, Engineering, and Life Sciences (except Biotechnology)
Contractor
Sierra Nevada Corporation (SIERRA NEVADA CORPORATION)
Contracting Agency/Office
National Aeronautics and Space Administration»Office of the Administrator
Effective date
08/29/2017
Obligated Amount
$24.2M
NNH17CS40C - THIS CONTRACT IS A RESULT OF A DOWNSELECT FROM AWARDS ISSUED AS A RESULT OF NNH15ZDA001N-S3GSI. A SUMMARY OF THE RESEARCH IS AS FOLLOWS: FUTURE ROBOTIC MISSIONS TO VENUS REQUIRE ACTUATORS FOR POWERING ROBOTIC ARMS, SAMPLING SYSTEMS, AND GIMBALS FOR THE POSITIONING OF CAMERAS AND ANTENNAS. THERE ARE MANY TYPES OF ACTUATORS (E.G. PNEUMATIC, HYDRAULIC); HOWEVER ELECTRIC ACTUATORS OFFER THE GREATEST VERSATILITY FOR SPACE MISSIONS. AN ELECTRIC ACTUATOR CONSISTS OF AN ELECTRIC MOTOR AND A POSITION SENSOR. THE ELECTRIC MOTOR CONVERTS ELECTRICAL ENERGY (ELECTRICITY) INTO MECHANICAL OUTPUT (SHAFT ROTATION). THE POSITION SENSOR, ON THE OTHER HAND, DETERMINES THE ANGULAR POSITION OF THE MOTOR SHAFT, WHICH THEN IS PROCESSED BY DRIVE ELECTRONICS TO COMMUTATE AND CONTROL THE MOTOR. BECAUSE OF THE EXTREME CONDITIONS ON THE VENUS SURFACE (92 BAR PRESSURE, 462 C TEMPERATURE, AND SUPERCRITICAL CO2 ATMOSPHERE), CONVENTIONAL ACTUATORS WILL NOT BE ABLE TO FUNCTION PROPERLY, OR AT ALL. THE MAIN CHALLENGES PERTAIN TO CHANGES IN ELECTRICAL PROPERTIES LIKE AN INCREASE IN WIRE RESISTANCE (LEADING TO GREATER LOSSES), CHANGES IN MAGNETIC PROPERTIES LIKE PERMEABILITY AND RETENTIVITY (LEADING TO DEMAGNETIZATION OF MAGNETS), AND CHANGES IN PHYSICAL PROPERTIES SUCH AS LINEAR EXPANSION, DECREASE IN STRENGTH, INCREASE IN FRICTION, AND ACCELERATED OXIDATION. HONEYBEE HAS DEVELOPED A 48V BRUSHLESS DC MOTOR (BLDC) AND CUSTOM POSITION SENSOR CALLED THE PULSED INJECTION POSITION SENSOR (PIPS) FOR MOTOR COMMUTATION AND FEEDBACK CONTROL. THE MOTOR AND PIPS ARE AT TECHNOLOGY READINESS LEVEL (TRL) 5. THE MAIN OBJECTIVE OF THE PROPOSED WORK IS TO MATURE THE VENUS ACTUATOR TECHNOLOGY THROUGH AN ITERATIVE PROCESS OF VENUS CHAMBER TESTING OF A TRL5 ACTUATOR, FOLLOWED BY RE-DESIGN AND FABRICATION OF A TRL6 ACTUATOR AND SUBSEQUENT VENUS CHAMBER QUALIFICATION TESTING OF THAT ACTUATOR. THE CRITICAL OBJECTIVES TO BE MET ARE AS FOLLOWS: 1. DESIGN OF A MOTOR WITH 28V WINDINGS, 2. INCREASE PIPS RESOLUTION (THIS WILL MAKE MOTOR MORE EFFICIENT AND ALLOW ACTUATOR TO BE USED FOR PRECISION POSITIONING SYSTEMS ROBOTIC ARMS AND GIMBALS), 3. ESTABLISH REPRODUCIBLE PROCEDURES, STANDARDS, AND GUIDELINES FOR FABRICATING, ASSEMBLY, TEST, AND INSPECTION OF VENUS ACTUATORS (CURRENTLY ACTUATORS ARE HAND CRAFTED BY SELECTED ENGINEERS THIS KNOWLEDGE NEEDS TO BE CAPTURED SO THAT ANY SKILLED PERSON WILL BE ABLE TO FABRICATE VENUS ACTUATOR WHENEVER NEEDED). THIS EFFORT WILL BE ACHIEVED IN ONE YEAR PERIOD TO ENABLE TECHNOLOGY INFUSION INTO THE NEW FRONTIERS (NF) VENUS IN SITU EXPLORER (VISE) MISSION.
Definitive Contract - 541712 Research and Development in the Physical, Engineering, and Life Sciences (except Biotechnology)
Contractor
HONEYBEE ROBOTICS, LTD. (HONEYBEE ROBOTICS, LTD)
Contracting Agency/Office
National Aeronautics and Space Administration»Office of the Administrator
Effective date
05/31/2017
Obligated Amount
$300k
NNH17CL01C - THE GOAL OF THIS RESEARCH IS TO CONDUCT A FEASIBILITY STUDY TO VALIDATE THE RELATIVE EASE AND AFFORDABILITY OF REPURPOSING ROCKET UPPER STAGES TO SERVE AS HABITATS, BEGINNING WITH A DEMONSTRATION OF CONVERTING AND ATTACHING A CENTAUR UPPER STAGE TO THE INTERNATIONAL SPACE STATION (ISS). THIS CONTRACT IS IN SUPPORT OF THE FOLLOWING LIST OF NASA OBJECTIVES FOR THIS PHASE OF THE HABITATION SYSTEM DEVELOPMENT: 1. DEVELOP AND REFINE THE EVOLVABLE, MODULAR ARCHITECTURE, FUNCTIONAL ALLOCATION OPTIONS, STANDARDS, AND COMMON INTERFACES REQUIRED TO ENABLE INTEROPERABILITY OF THE AGGREGATE SYSTEM TO PROVIDE LONG DURATION DEEP SPACE TRANSIT HABITATION. ACHIEVE A LEVEL OF FIDELITY IN TECHNICAL AND PROGRAMMATIC FEASIBILITY CONCEPTS FOR GROUND PROTOFLIGHT VEHICLES-MODULES-UNITS/ 2. FURTHER DEFINE AND DEVELOP DEEP SPACE HABITATION CAPABILITIES THAT CAN BE FLOWN AS CO-MANIFESTED PAYLOADS ON SLS BLOCK 1B WITH AN INITIAL SLS CO-MANIFESTING CAPABILITY OF 4 TO 6 METRIC TONS STARTING IN EARLY-TO-MID 2020S, OR LATER IN THE 2020S ON A CARGO-ONLY VERSION OF SLS, OR ON ALTERNATIVE LAUNCH VEHICLES. NOTE THE HABITATION SYSTEM CONCEPT CAN BE SEPARATED INTO MULTIPLE INTEGRATED MODULES WITH DISTRIBUTED FUNCTIONS. IF THE HABITATION CONCEPT IS NOT FLOWN ON SLS, PROVIDE DETAILS OF THE LAUNCH VEHICLE ASSUMPTIONS. 3. MATURE THE DESIGN OF THE OVERALL DEEP SPACE INTEGRATED SYSTEM(S) AND, AT A MINIMUM, DEVELOP A FULL SIZE, GROUND PROTOTYPE OF THE PORTION OF YOUR DESIGN THAT PROVIDES THE MAJORITY OF THE HABITATION CAPABILITIES FOR FORM, FIT, AND PARTIAL FUNCTION INTEGRATION TESTING. 4. IDENTIFY COMMERCIAL CAPABILITY DEVELOPMENT FOR LEO THAT INTERSECTS NASA LONG DURATION DEEP SPACE HABITATION REQUIREMENTS ALONG WITH ANY POTENTIAL OPTION TO MAXIMIZE THE LEVERAGING OF COMMERCIAL LEO ADVANCEMENTS TOWARDS MEETING NASA LONG DURATION DEEP SPACE HABITATION NEEDS. 5. PROVIDE INFORMATION ON COMPANY END-TO-END DEVELOPMENT EFFORT AND ROM COSTS FOR FLIGHT DEVELOPMENT - COMPANIES TO PROVIDE A PROPOSAL, SOW, AND FULLY PRICED APPENDIX A EFFORTS AND ROM COSTS FOR SUBSEQUENT PHASES FOR ENGINEERING AND FLIGHT UNIT DEVELOPMENT. THIS CONTRACT IS FOR THE LXION TEAM TO COMPLETE BOTH THE PHASE 1 AND PHASE 2 WORK IN A RAPID, EFFICIENT, AND JUDICIOUS MANNER, FINISHING BOTH THE CORE FEASIBILITY AND THE CONCEPT/ARCHITECTURE PHASES OF THE STUDY BEFORE THE END OF CALENDAR YEAR 2017. THIS WILL ALLOW THE LXION TEAM TO QUICKLY MOVE INTO DEVELOPING HARDWARE, INCLUDING OUTFITTING AN ACTUAL CENTAUR IN EARLY 2018, AND BEING READY FOR THE FIRST FLIGHT OF THE LXION HABITAT AS EARLY AS 2020. THE FOCUS OF THE IXION INITIATIVE PROPOSAL IS TO DEVELOP AND DEMONSTRATE THE CAPABILITY TO REPURPOSE PROPELLANT TANKS INTO HABITABLE VOLUMES ON-ORBIT FOR USE IN AN OVERALL IN-SPACE ARCHITECTURE. THE CAPABILITY WILL BE DEMONSTRATED IN TWO PHASES. FIRST IS A CORE FEASIBILITY STUDY AS PHASE 1 AND THEN THE IXION TEAM WILL PLAN A COMPREHENSIVE SYSTEMS CONCEPTS AND ARCHITECTURE STUDY FOR PHASE 2 SHOULD THE FEASIBILITY STUDY MERIT SUCH FURTHER WORK. REPORTS WILL INCLUDE COST-BENEFIT ANALYSES OF REPURPOSING STRATEGIES AND TECHNIQUES THAT ARE MOST ATTRACTIVE. A CON-OPS MEDIA PRESENTATION WILL BE DEVELOPED THROUGHOUT BOTH PHASES 10 ILLUSTRATE THE STRATEGY AND WILL BE ADDED TO AND ENHANCED AS THE PROJECT PROGRESSES.
Definitive Contract - 541712 Research and Development in the Physical, Engineering, and Life Sciences (except Biotechnology)
Contractor
NANORACKS, LLC
Contracting Agency/Office
National Aeronautics and Space Administration»Office of the Administrator
Effective date
05/01/2017
Obligated Amount
$11.2M
NNH16CT04C - NASA RESEARCH ANNOUNCEMENT AWARD. THE GOAL OF THIS RESEARCH EFFORT IS TO CREATE A NEW LANGUAGE OF HIGHLY DESCRIPTIVE TERMINOLOGY AND VISUALIZATION COMPONENTS THAT AUGMENT EXISTING EFFORTS TO DESCRIBE THESE INCREASINGLY AUTONOMOUS (IA) SYSTEMS. THESE NEW TOOLS, TECHNIQUES, AND METHODOLOGY FOR DESCRIBING AND COMMUNICATING COMPLEX IA SYSTEMS HELP TO ADDRESS A CRITICAL GAP IN THE ENGINEERING ENVIRONMENT WHERE GREATER PRECISION, BREADTH, AND TRACEABLE DESCRIPTION IS NEEDED IN THE REQUIREMENTS DEVELOPMENT PHASE. GREATER AWARENESS AND PLANNING FOR DIVERSE VIEWPOINTS AND CRITICAL STAKEHOLDER FACTORS ARE EXPECTED TO PREEMPTIVELY ADDRESS DESIGN CHALLENGES EARLIER IN THE PROCESS. IT IS EXPECTED THAT THESE RESEARCH FINDINGS WILL BE PARTICULARLY RELEVANT AND SIGNIFICANT TO NASA AS THIS CONTRACT WILL FRAME THE RESEARCH WITHIN A FOCUSED IA SYSTEMS DEVELOPMENT USE CASE SCENARIO OF ON-DEMAND COMMERCIAL DELIVERY OF CONSUMER PRODUCTS VIA UNMANNED AIRCRAFT SYSTEMS. THIS USE CASE WILL ALLOW OUR RESEARCH TO BE GERMANE TO AN EXAMPLE IA SYSTEM, DEMONSTRATE HOW OUR APPROACH MIGHT BE PRACTICALLY APPLIED, AND PROVIDE A CLEAR INDICATION OF POTENTIAL BENEFITS FROM SUCCESSFUL COMPLETION OF THIS RESEARCH.
Definitive Contract - 541712 Research and Development in the Physical, Engineering, and Life Sciences (except Biotechnology)
Contractor
Logistics Management Institute (LOGISTICS MANAGEMENT INSTITUTE)
Contracting Agency/Office
National Aeronautics and Space Administration»Office of the Administrator
Effective date
08/16/2016
Obligated Amount
$962.9k
NNH16CE01B - STUDIES RELATING TO AERONAUTICS AND SPACE PROGRAMS AND SYSTEMS ENGINEERING.
IDC - 541990 All Other Professional, Scientific, and Technical Services
Contractor
National Academy of Sciences (NATIONAL ACADEMY OF SCIENCES)
Contracting Agency/Office
National Aeronautics and Space Administration»Office of the Administrator
Effective date
08/15/2016
Obligated Amount
$10M
NNH16CW21P - - NATIONAL SOCIETY OF BLACK ENGINEERS (NSBE) AEROSPACE SYSTEMS CONFERENCE SPONSORSHIP.
Purchase Order - 511199 All Other Publishers
Contractor
NATIONAL SOCIETY OF BLACK ENGINEERS
Contracting Agency/Office
National Aeronautics and Space Administration»Office of the Administrator
Effective date
05/19/2016
Obligated Amount
$8k
NNH16PB26P - SYSTEM ENGINEERING, STANDARDIZATION AND SOFTWARE ARCHITECTURE SUPPORT TO THE DELAY/DISRUPTION TOLERANT NETWORKING PROJECT IN THE ADVANCE EXPLORATION SYSTEM DIVISION AS WELL AS KNOWLEDGE AND INVOLVEMENT IN THE CONSULTATIVE COMMITTEE ON SPACE AND DATA SERVICES (CCSDS). .
Purchase Order - 541990 All Other Professional, Scientific, and Technical Services
Contractor
The Mitre Corporation (THE MITRE CORPORATION)
Contracting Agency/Office
National Aeronautics and Space Administration»Office of the Administrator
Effective date
01/12/2016
Obligated Amount
$155.3k
NNH15CN86C - NASA BROAD AGENCY ANNOUNCEMENT AWARD NNH15ZCQ001K. THE OBJECTIVES OF THIS WORK ARE TO DEMONSTRATE AND MEASURE KEY TECHNICAL FUNCTIONS AND PARAMETERS RELEVANT TO NASA. AD ASTRAS WELL DEMONSTRATED EXPERIMENTAL AND ENGINEERING DEVELOPMENT PRACTICES WILL BE FOLLOWED THROUGHOUT THE PROJECT. AD ASTRA WILL DEMONSTRATE THE FOLLOWING POWER. AD ASTRA WILL PERFORM OPERATIONAL THERMAL STEADY STATE TESTS IN A DESIGN THAT IS EFFICIENT AND EXTENSIBLE TO CONTINUOUS OPERATIONS PER THRUSTER. TRL 5 PPUS. AD ASTRA WILL USE EXISTING TRL5 RADIO FREQUENCY GENERATORS (RF PPUS) THAT WERE DEVELOPED AND BUILT BY NAUTEL LTD AND PROVEN IN VX 200 TESTING. THESE PPUS ARE RATED FOR STEADY STATE OPERATION, HAVE ALREADY DEMONSTRATED A COMBINED EFFICIENCY PERCENTAGE AND A SPECIFIC MASS. LIFETIME. AD ASTRA WILL CARRY OUT 100 HOURS CONTINUOUS LIFETIME TESTING FOR THE FULL 100 HOURS AT FULL THERMAL STEADY STATE. AD ASTRA WILL PERFORM EROSION MEASUREMENTS AT THE END OF THE TEST WITH A PRECISION GOAL SUFFICIENT TO EXTRAPOLATE OPERATIONAL (THRUSTING) LIFETIME TO A NUMBER OF HOURS. PERFORMANCE. AD ASTRA WILL MEASURE ROCKET PERFORMANCE USING VX 200 PEER REVIEWED PUBLISHED TECHNIQUES IN EACH PHASE OF THE PROJECT. PERFORMANCE MEASUREMENTS MADE DURING LONG DURATION STEADY STATE OPERATIONS DRIVE COST. EXCLUDING THE LABORATORY SUPERCONDUCTING MAGNET COOLING POWER, AD ASTRA WILL VERIFY A SYSTEM EFFICIENCY GOAL OF GREATER THAN 60 PERCENT, INCLUDING THE RF PPUS, AT A SPECIFIC IMPULSE OF INTEREST USING ARGON PROPELLANT. AD ASTRA WILL ALSO CARRY OUT VARIABLE SPECIFIC IMPULSE TESTING WITHIN A RANGE. THESE TESTS WILL ALLOW TRL 6 DESIGNS THAT WILL ACHIEVE TOTAL SYSTEM EFFICIENCY GREATER THAN 60 PERCENT IN THE SPECIFIC IMPULSE RANGE OF 2000 S TO 5000 S USING HIGH TEMPERATURE SUPERCONDUCTORS WITH ARGON AND KRYPTON PROPELLANTS.
Definitive Contract - 541712 Research and Development in the Physical, Engineering, and Life Sciences (except Biotechnology)
Contractor
AD ASTRA ROCKET COMPANY
Contracting Agency/Office
National Aeronautics and Space Administration»Office of the Administrator
Effective date
08/07/2015
Obligated Amount
$8.9M
NNH15PY87P - ENGINEERING AND TECHNICAL SERVICES: SITE SURVEY FOR JOHNSON SPACE CENTER/FOR A HF AUTOMATIC LINK ESTABLISHMENT TRANSCEIVER COMMUNICATION SYSTEM.
Purchase Order - 541330 Engineering Services
Contractor
Raytheon (RTX) (ROCKWELL COLLINS SERVICES, COMPANY)
Contracting Agency/Office
National Aeronautics and Space Administration»Office of the Administrator
Effective date
04/14/2015
Obligated Amount
$11.3k
NNH14CL75C - CT PROGRAM: ASTEROID REDIRECT MISSION (ARM). PROJECT: ADAPTING COMMERCIAL SPACECRAFT FOR THE ARM. THIS PROJECT WILL STUDY THE FEASIBILITY OF ADAPTING AND LEVERAGING COMMERCIAL SPACECRAFT DESIGN, MANUFACTURE, INTEGRATION, AND TESTING CAPABILITIES FOR DEVELOPING THE ASTEROID REDIRECT VEHICLE. A FEASIBILITY STUDY ON THE USE OF EXISTING COMMERCIAL DESIGNS FOR THE ARV AND/OR MISSION MODULE SHALL BE PREPARED, INCLUDING ANY MODIFICATIONS REQUIRED TO EXISTING COMMERCIAL DESIGNS, THE LEVERAGING OF COMMERCIAL DEVELOPMENT AND FABRICATION CAPABILITIES, AND INTEGRATION AND TESTING FACILITIES. THE STUDY SHALL INCLUDE CONCEPTUAL SYSTEMS DESIGN, ANALYSIS, AND ENGINEERING, AND AN ESTIMATE OF THE COST AND SCHEDULE REQUIRED FOR FLIGHT SYSTEMS DEVELOPMENT. INNOVATIVE IDEAS FOR MINIMIZING COST TO THE GOVERNMENT ARE ENCOURAGED. THE CONTRACTOR WILL PERFORM TRADE STUDIES, DESIGN WORK, AND ANALYSIS TO SUPPORT CONCEPTUAL SPACECRAFT DESIGN SUITABLE FOR THE ARM MISSION AS DESCRIBED IN THE BAA. PROVIDE COST AND SCHEDULE ANALYSIS FOR THE FLIGHT SYSTEM DEVELOPMENT THAT INCLUDES CONSIDERATION OF ALTERNATIVE PROCUREMENT APPROACHES. THE CONTRACTOR SHALL PERFORM SYSTEMS ENGINEERING TRADE STUDIES, ANALYSIS, AND SUPPORT FOR THE ARM SPACECRAFT DESIGN AND PROPULSION MODULE INCLUDING THE INTERFACE WITH THE CAPTURE SYSTEM. REQUIREMENTS SHALL BE DEVELOPED CONSISTENT WITH THOSE STATED IN SECTION 1.0 AND SYSTEM DESIGN CHOICES SHALL BE TRACEABLE TO THESE REQUIREMENTS. A MASTER EQUIPMENT LIST SHALL BE COMPILED USING THE GOVERNMENT FURNISHED TEMPLATE. THE CONTRACTOR SHALL DESIGN, CONFIGURE, AND BUILD STRUCTURAL MODELS THAT PROVIDE PROPER INTERFACES FOR ALL SPACECRAFT SUBSYSTEMS AND MEET STATIC AND DYNAMIC STRENGTH REQUIREMENTS FOR THE ARM SPACECRAFT. THE CONTRACTOR SHALL PERFORM SYSTEMS ENGINEERING TRADE STUDIES TO DETERMINE HOW BEST TO MAKE THE ARM VEHICLE EXTENSIBLE TO OTHER IMPORTANT NASA MISSIONS. THE CONTRACTOR SHALL ENSURE THAT THE SUBSYSTEM BEING DEVELOPED MEETS THE NEEDS OF ALL VARIANTS OF THE BASIC ARM VEHICLE. THE CONTRACTOR SHALL PERFORM ASSEMBLY, TEST, LAUNCH AND OPERATIONS (ATLO) TRADE STUDIES, ANALYSIS AND DESIGN FOR THE SEP AND COMBINED PROPULSION AND MISSION MODULE, INCLUDING A REVIEW OF THE ATLO PLAN, DEFINITION OF A SPACECRAFT BUILD FLOW, AND LONG-LEAD HARDWARE DETERMINATION. THE CONTRACTOR SHALL PERFORM GUIDANCE NAVIGATION AND CONTROL TRADE STUDIES, ANALYSIS AND DESIGN FOR THE COMBINED PROPULSION AND MISSION MODULE.
Definitive Contract - 336414 Guided Missile and Space Vehicle Manufacturing
Contractor
Lockheed Martin Corporation (LOCKHEED MARTIN CORPORATION)
Contracting Agency/Office
National Aeronautics and Space Administration»Office of the Administrator
Effective date
08/25/2014
Obligated Amount
$443.6k

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