Awards for “BAE SYSTEMS SPACE & MISSION SYSTEMS INC.”
25 awards on this page · sorted by amount · page 10
| Award ID | Recipient | Awarding agency | Amount | Start | End | NAICS | Description |
|---|---|---|---|---|---|---|---|
| NNL08AA43C | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | National Aeronautics and Space Administration | $485.68K | 2008-08-01 | 2009-11-30 | 541712 | STATEMENT OF WORK FOR SHARED-APERTURE ZOOM OPTICS SUBSYSTEM FOR A FLASH LIDAR LANDING SENSOR 1.0 INTRODUCTION/BACKGROUND: THE ALHAT PROJECT HAS BEEN ESTABLISHED TO PROVIDE AN AUTONOMOUS LUNAR LANDING SYSTEM FOR CREWED, CARGO, AND ROBOTIC LUNAR DESCENT VEHICLES. THE ALHAT SYSTEM WILL ENABLE GLOBAL LUNAR ACCESS FOR EXPLORATION OF AREAS ON THE LUNAR SURFACE NEVER BEFORE VISITED, WITHOUT REGARD TO LIGHTING CONDITIONS. THE ALHAT SYSTEM WILL BE CAPABLE OF LANDING A LUNAR DESCENT VEHICLE WITHIN REQUIRED PRECISION AND ACCURACY OF A PRE-DESCENT DESIGNATED LANDING LOCATION. THIS INTEGRATED SYSTEM INCLUDES DEDICATED LANDING SENSORS, COMPUTATIONAL ALGORITHMS, AND AN INTERFACE TO A LANDING VEHICLE COMMAND AND DATA HANDLING SYSTEM THAT ULTIMATELY WILL BE IN CONTROL OF THE LANDING VEHICLE. THE SCOPE OF THE ALHAT PROJECT INCLUDES THE DEFINITION, DESIGN, DEVELOPMENT, TEST, VERIFICATION, AND VALIDATION (V&V) OF AN INTEGRATED GUIDANCE, NAVIGATION AND CONTROL (GNC) LUNAR DESCENT AND LANDING SYSTEM CONSISTENT WITH TECHNOLOGY READINESS LEVEL (TRL) 6. THE ALHAT SYSTEM IS EXPECTED TO BE APPLICABLE TO A VARIETY OF VEHICLE TYPES, BOTH CREWED AND NON-CREWED. THE AUTONOMOUS LANDING SCENARIOS DRIVE THE REQUIREMENTS FOR LANDING SENSOR ACCURACY AND RELIABILITY (SAFE AND PRECISE). THE CREWED SCENARIOS DRIVE THE NEED TO PROVIDE INFORMATION AT VIDEO RATES (1 30 HZ) FOR USE SIMILAR TO A HEADS UP DISPLAY TO ALLOW CREW INTERFACE AND TO FACILITATE PROVISIONS FOR MANUALLY CONTROLLED LANDINGS. BOTH SCENARIOS COULD BE ACHIEVED USING A SINGLE INTEGRATED SENSOR SYSTEM, BUT FURTHER DEVELOPMENT OF CERTAIN KEY TECHNOLOGIES IS NEEDED FOR MEETING THE ALHAT OBJECTIVES. TO MEET THE SAFE AND PRECISE LANDING REQUIREMENTS, THE ALHAT SYSTEM WILL MAKE USE OF THE 3-D IMAGING SENSOR DATA TO DETECT AND AVOID POTENTIAL LANDING HAZARDS DURING THE FINAL STAGES OF THE POWERED DESCENT FOR LUNAR LANDING. THE ALHAT SYSTEM LANDING SENSOR AND ASSOCIATED ALGORITHMS WILL BE CAPABLE OF DETECTING AND LOCATING LANDING HAZARDS SUCH AS ROCKS, CRATERS, SLOPES OR OTHER DISCONTINUOUS SURFACE FEATURES. THIS ABILITY TO DETECT AND LOCATE HAZARDS WILL ENABLE THE POTENTIAL FOR TRAJECTORY RETARGETING AND MANEUVERING TO A SAFE LANDING SITE. THE SIMULTANEOUS ACQUISITION AND LOCATION DETERMINATION OF HAZARDS AND CONVERSELY, ACQUISITION AND LOCATION DETERMINATION OF SAFE LANDING SITES, ALONG WITH THE RELATIVE POSITION INFORMATION INHERENT IN THE 3-D IMAGE, WILL ENABLE THE PRECISION NAVIGATION NECESSARY BOTH TO AVOID HAZARDS AND LAND PRECISELY AT THE RETARGETED LOCATION. NASA RESEARCH ANNOUNCEMENT (NRA) NNL08ZD2001N ENTITLED LANDING SENSOR ADVANCED COMPONENT TECHNOLOGIES SOLICITED PARTNERS TO RESEARCH, DEVELOP, AND DEMONSTRATE COMPONENT- AND SUBSYSTEM-LEVEL TECHNOLOGIES SPECIFICALLY RELATED TO ALHAT THAT WILL INCREASE PERFORMANCE, REDUCE RISK, COST, SIZE, AND MASS OF A STATE OF THE ART SENSOR CAPABLE OF ENABLING A DESCENT VEHICLE TO AUTONOMOUSLY PERFORM A SAFE AND ACCURATE LANDING. THE BASIC TECHNOLOGY CHOSEN FOR THIS SENSOR IS FLASH LIDAR. FLASH LIDAR PROVIDES A 3-D IMAGING CAPABILITY WHICH CAN BE EXPLOITED TO GENERATE THE NECESSARY INFORMATION FOR ACCURATE NAVIGATION BY IMPLEMENTATION OF APPROPRIATE REAL TIME SIGNAL AND/OR IMAGE PROCESSING TECHNIQUES. THE GOAL IS TO ADVANCE THE CORE SENSOR COMPONENT TECHNOLOGIES TO A TECHNOLOGY READINESS LEVEL THAT ENABLES THEIR EVENTUAL INFUSION INTO FUTURE SPACE FLIGHT MISSIONS. THE SOLICITED COMPONENT AND SUBSYSTEM-LEVEL TECHNOLOGY AREAS SOLICITED BY THE NRA FOR FURTHER ADVANCEMENT WERE AS FOLLOWS:  DETECTOR FOCAL PLANE ARRAYS  READ OUT INTEGRATED CIRCUITS (ROIC)  3-D IMAGE PRE-PROCESSING AND ENHANCEMENT  VARIABLE FOCAL LENGTH OPTICS  IMPROVED LASER PERFORMANCE FOR FLASH LIDAR APPLICATIONS BALL AEROSPACE & TECHNOLOGIES CORPORATION S PROPOSAL ENTITLED, SHARED-APERTURE ZOOM OPTICS SUBSYSTEM FOR A FLASH LIDAR LANDING SENSOR, WAS SELECTED FOR AWARD UNDER THE TECHNOLOGY TOPIC AREA OF VAR |
| NNL08AA34C | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | National Aeronautics and Space Administration | $481.22K | 2008-03-28 | 2010-06-01 | 541712 | PERFORMANCE AND CONFIGURATION STUDY OF DEPLOYABLE HIGH MASS MARS ENTRY SYSTEMS |
| SPM7M910M0008 | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | Department of Defense | $478.48K | 2009-10-15 | 2010-06-12 | 334220 | 4512260246!ANTENNA |
| SPM7M909C0017 | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | Department of Defense | $475.55K | 2009-04-10 | 2010-05-08 | 334220 | 4510458719!ANTENNA |
| SPE7M519P7879 | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | Department of Defense | $471.85K | 2019-06-03 | 2020-09-08 | 334220 | 8506558789!ANTENNA |
| 80LARC23F0015 | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | National Aeronautics and Space Administration | $471.81K | 2022-11-22 | 2023-11-22 | 541330 | SUSTAIN ENGINEERING SUPPORT FOR THE CALIPSO MISSION INCLUDING THE PAYLOAD DATA DELIVERY SYSTEM AND THE WORK PERFORMED BY THE CALIPSO MISSION OPERATION CONTROL CENTER FOR BOTH THE OPERATIONAL (PHASE E) AND CLOSEOUT PHASE (PHASE F) OF THE MISSION |
| NNL11AB64T | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | National Aeronautics and Space Administration | $469.84K | 2011-04-20 | 2011-12-31 | 541712 | STRATOSPHERIC AEROSOL AND GAS EXPERIMENT REFURBISHMENT ANALYSIS AND SUPPORT |
| SPM7M908M4134 | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | Department of Defense | $458.55K | 2008-05-30 | 2009-01-25 | 339999 | 4507739832!ANTENNA |
| NNH14CL73C | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | National Aeronautics and Space Administration | $449.94K | 2014-07-25 | 2015-08-27 | 336414 | IGF::CT::IGF BAA ENTITLED "RENDEZVOUS SENSOR SUITE DEVELOPMENT" THE CONTRACTOR SHALL COMPLETE THE FOLLOWING EFFORTS: 1. PROGRAM MANAGEMENT AND SYSTEMS ENGINEERING 2. VNS UPGRADES 3. VISIBLE CAMERA UPGRADES 4. IR CAMERA DESIGN THE CONTRACTOR SHALL PERFORM OVERALL SYSTEMS ANALYSIS AND INTEGRATION OF INDIVIDUAL SENSOR DEVELOPMENT TASKS, INCLUDING CONDUCTING TRADES AND DEFINING REQUIREMENTS AND GOALS AS NEEDED TO COMPLETE THE TASKS DEFINED IN THIS SOW. THIS INCLUDES DEFINING REQUIREMENTS AND DESIGN FEATURES THAT ENSURE LOOSELY INTEGRATED SENSOR SUITE CHARACTERISTICS ARE ACHIEVED WHILE ALSO ENABLING PROGRESSION TO A TIGHTLY INTEGRATED SENSOR SUITE. RESULTS INCLUDE DEFINITION OF PREFERRED ARCHITECTURES FOR THE ENTIRE SENSOR SUITE AND HOW THE SENSOR SUITE CAN BE MODULARIZED AND PROGRESS FROM LOOSELY INTEGRATED TO HIGHLY INTEGRATED, INCLUDING CONSIDERATION OF HOW HIGHER LEVEL ALGORITHMS, DATA PROCESSING, AND SENSOR SUITE CONTROL COULD BE INCORPORATED. THE CONTRACTOR SHALL PARTICIPATE IN MEETINGS AND REVIEWS AS REQUIRED. THE CONTRACTOR SHALL DEVELOP ELECTRICAL DESIGN MODIFICATIONS TO REDUCE ESFL POWER CONSUMPTION FROM 90 W TO A GOAL OF LESS THAN 5 W. THE CONTRACTOR WILL IMPLEMENT THE DESIGN MODIFICATIONS ON THEIR EXISTING ESFL BRASS BOARD HARDWARE, DEMONSTRATE ESFL OPERATION OF THE MODIFIED HARDWARE, AND MEASURE NEW POWER CONSUMPTION. THE RESULTS OF THIS DEMONSTRATION WILL BE DE-SCRIBED IN THE FINAL REPORT. THE CONTRACTOR SHALL DEVELOP AN OPTOMECHANICAL PACKAGE DESIGN FOR THE AOBD CRYSTAL USED IN THEIR ESFL TECHNOLOGY. THE RESULTING DESIGN SHALL BE ABLE TO SURVIVE SHOCK, THERMAL, VIBRATION, AND VACUUM ENVIRONMENTS REQUIRED FOR SPACE FLIGHT. THIS PACKAGE DESIGN WILL BE DESCRIBED IN THE FINAL REPORT. THE CONTRACTOR SHALL UPDATE THE VNS MECHANICAL DESIGN TO ENHANCE MODULARITY AND PERFORMANCE FOR THE ARM MISSION REQUIREMENTS. SPECIFIC ITEMS THAT COULD BE INCLUDED ARE: INCORPORATION OF ESFL COMPONENTS, ENABLING DIFFERENT RECEIVE OPTICS OPTIONS, AND ENABLING DIFFERENT LASER OPTIONS. END PRODUCT IS CAD MODEL OF UPDATED VNS SHOWING DESIGN CHANGES AND THE VARIOUS MODULAR CONFIGURATIONS ENABLED. THE RESULT OF THIS UPDATED CAD MODEL WILL BE INCLUDED IN THE FINAL RE-PORT. THE CONTRACTOR SHALL DEFINE VNS ELECTRICAL SUBSYSTEM MODIFICATIONS REQUIRED TO ENHANCE MODULARITY AND PERFORMANCE FOR THE ARM MISSION REQUIREMENTS. END PRODUCT IS UPDATED BLOCK DIAGRAMS TO DRIVE EVENTUAL ELECTRONIC BOARD DESIGN UPDATES. THE UPDATED BLOCK DIAGRAMS WILL BE INCLUDED IN THE FINAL REPORT. THE CONTRACTOR SHALL DEFINE UPDATES TO THEIR EXISTING ORION DOCKING CAMERA DESIGN TO ENHANCE MODULARITY AND PERFORMANCE. END PRODUCTS INCLUDE UPDATED CAD MODEL AND BLOCK DIAGRAMS. THE RESULT OF THIS UPDATED CAD MODEL AND THE BLOCK DIAGRAMS WILL BE INCLUDED IN THE INTERIM BRIEFING OR FINAL REPORT. THE CONTRACTOR SHALL DEVELOP AN INITIAL IR CAMERA DESIGN TO MEET ARM REQUIREMENTS LEVERAGING THEIR BESST INSTRUMENT AND DOCKING CAMERA. THE END GOAL IS AN IR CAMERA DESIGN THAT HAS A VERY SIMILAR COMMAND, TELEMETRY, DATA, AND OPERATIONAL PROCEDURES AS THE EXISTING DOCKING CAM-ERA BUT THAT OUTPUTS IR IMAGES. THIS TASK INCLUDES A SURVEY OF POTENTIAL SOURCES OF MICRO-BOLOMETER ARRAYS, DEVELOPMENT OF THE SPECIFICATION FOR THE IR CAMERA, AND A PRELIMINARY CAMERA DESIGN PACKAGE. THE RESULTS OF THE SURVEY, SPECIFICATION, AND PRELIMINARY CAMERA DESIGN PACKAGE WILL BE DESCRIBED IN THE INTERIM BRIEFING OR THE FINAL REPORT. |
| 0015 | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | Department of Defense | $449.53K | 2005-09-20 | 2010-03-31 | 541710 | 200511!004071!5700!FA8650!DET 1 AFRL/PK !F3361501D1844 !A!N! !Y!0015 ! !20050920!20060920!085270270!926451519!006419147!N!BALL AEROSPACE & TECHNOLOGIES !1600 COMMERCE ST !BOULDER !CO!80301!07850!013!08!BOULDER !BOULDER !COLORADO !+000000026200!N!N!000000000000!AC62!RDTE/ELECTRONICS & COMMUNICATION EQ-APPLIED RESEA !A7 !ELECTRONICS AND COMMUNICATION EQUIP !000 !* !541710!E! !4! ! ! ! ! !20200930!B! ! !A! !A!N!U!2!002!N!1A!Z!N!Z! ! !N!C!N! ! ! !Z!Z!A!A!000!A!C!N! ! ! ! ! ! !0001! ! |
| FA945303C0237 | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | Department of Defense | $433.47K | 2003-10-27 | 2010-09-16 | 541710 | 200411!000041!5700!GS05 !DET 8 AFRL/PK (SUPPORTS VS) !FA945303C0237 !A!N! !N! ! !20031027!20040602!926451519!926451519!006419147!N!BALL AEROSPACE & TECHNOLOGIES !1600 COMMERCE STREET !BOULDER !CO!80306!07850!013!08!BOULDER !BOULDER !COLORADO !+000000436652!N!N!000000436652!AC23!RDTE/MISSILE AND SPACE SYSTEMS-ADV TECH DEV !A2 !MISSILE AND SPACE SYSTEMS !CAA !MDA SUPPORT !541710!E! !3! ! ! ! ! !99990909!B! ! !B! !A!N!U!2!001!E! !Z!Y!Z! ! !N!C!N! ! ! !C!C!A!A!000!A!B!N! ! ! ! ! ! !0001! ! |
| SPE7M518C0039 | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | Department of Defense | $430.97K | 2018-08-13 | 2019-05-10 | 334220 | 8505708748!ANTENNA |
| SPE7M517C0025 | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | Department of Defense | $419.34K | 2017-01-23 | 2018-02-20 | 334220 | 8503996436!ANTENNA |
| NNC09QA14P | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | National Aeronautics and Space Administration | $413.67K | 2009-04-24 | 2009-10-30 | 336415 | TANK-APPLIED MULTI-LAYER INSULATION SYSTEM |
| NNG10FD60C | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | National Aeronautics and Space Administration | $410K | 2009-10-14 | 2010-09-30 | 541330 | JOINT DARK ENERGY MISSION (JDEM) TELESCOPE CONCEPT STUDY. DETERMINE FEASIBLE TELESCOPE CONCEPTS FOR THE PRELIMINARY JDEM SCIENCE REQUIREMENTS AND ASSESS THE CRITICAL THERMAL, OPTICAL, MECHANICAL AND DYNAMIC ENVIRONMENTS THAT DRIVE THE JDEM TELESCOPE DESIGN. |
| 1332KP20CNEEP0078 | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | Department of Commerce | $401K | 2020-05-12 | 2020-12-11 | 541715 | BALL OPERATIONAL WEATHER INSTRUMENT EVOLUTION (BOWIE) LEO IR SOUNDER STUDY |
| FA861620F1003 | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | Department of Defense | $400.4K | 2020-07-09 | 2021-09-30 | 336411 | B-2 ANTENNA PROGRAM SUPPORT |
| 0004 | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | Department of Defense | $399.87K | 2010-09-30 | 2011-12-31 | 541330 | LABOR ARMY OPIR PRIORITY TASK |
| 0055 | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | Department of Defense | $398.79K | 2006-09-14 | 2011-05-31 | 541710 | SPECIAL STUDY |
| SPE7M125P9105 | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | Department of Defense | $392.55K | 2025-07-29 | 2026-10-28 | 334220 | 8511511908!ANTENNA |
| 0056 | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | Department of Defense | $390.4K | 2011-10-17 | 2013-09-30 | 541710 | DE-ORBIT CAPABILITY STUDY |
| HSCG3810P011088 | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | Department of Homeland Security | $390.17K | 2010-01-22 | 2010-11-19 | 336413 | HC144 MSP SPARES |
| NNG10AZ29D | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | National Aeronautics and Space Administration | $385K | 2010-06-08 | 2010-08-20 | 336414 | ICESAT-2 SPACECRAFT ACCOMMODATION STUDY |
| FA852717F0033 | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | Department of Defense | $383.32K | 2016-12-30 | 2017-08-25 | 541330 | IGF::CT::IGF AIRBORNE CUEING AND EXPLOITATION SYSTEM HYPERSPECTRAL JUON EFFORT IN SUPPORT OF THE AIR FORCE DISTRIBUTED GROUND SYSTEMS |
| N0001408C0595 | BAE SYSTEMS SPACE & MISSION SYSTEMS INC. | Department of Defense | $380.08K | 2008-09-26 | 2011-09-30 | 541712 | RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES (EXCEPT BIOTECHNOLOGY) |