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Mission Data Transmitters
L3 Cincinnati Electronics (L3 CE) offers a wide choice of modulators and transmitters for spacecraft ranging from X-Band to Ku-Band. All the products listed below can be customized to specific user requirements.
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SPARCv8 Software Development Environment
SPARCv8-SDE
The SPARCv8 Software Development Environment (SPARCv8-SDE) from STAR-Dundee is designed to support the development of software for the SPARC V8 series of processors, SoC devices and FPGA cores targeted for on-board spacecraft. SPARCv8-SDE consists of an all-in-one software development environment that provides great flexibility allowing generic application software development and, through a library of plugins, processor specific software.
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Three-Axis Satellite Magnetometers
TAM-1 Series
Macintyre Electronic Design Associa
The TAM-1 series of three-axis satellite magnetometers satisfies a broad range of spacecraft attitude determination and control applications. The basic TAM-1 design, which is based on rugged and reliable fluxgate magnetometer technology, has a long history of success in space. It has been used on numerous civilian and military satellites since the early 1970's.
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UHF Transceivers
Is designed to provide a wireless RF link between two orbiting spacecraft or other crafts such as a Lander on the surface of Mars, and an Orbiter craft orbiting above. The purpose of these transceivers is to facilitate the passing of data and commands between the two craft.
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Accelerometers
Columbia Research Laboratories
An instrument for measuring acceleration, typically that of an automobile, ship, aircraft, or spacecraft, or that involved in the vibration of a machine, building, or other structure.
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Qualification Testing
Qualification testing is an important step in evaluating how well spacecraft and launch vehicles perform under severe loading conditions that occur during launch and operation. ATA has conducted acoustic and vibration qualification testing of numerous launch vehicles and spacecraft components.
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Qualification Testing
Qualification, functional, and operational testing are important steps in evaluating how well spacecraft, launch vehicles, and other mechanical/electrical systems perform under severe loading conditions that occur during launch and operation.
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Power Special Test Equipment
PSTE
AMETEK Programmable Power, Inc.
There are several key benefits of the PSTE. First, it is a complete turnkey system that is capable of operating locally through a simple GUI interface or remotely via a host computer as a single Ethernet address. The spacecraft engineer who defines the spacecraft power bus limits, cabling scheme, mode simultaneity matrix, and system behavior based upon limit conditions implements the real intelligence of the system. From this definition, operating procedures can be generated to allow spacecraft technicians to operate the system, system protections are implemented that perform cable detection and mode verification, automated spacecraft fixture identification and related mode capability, and more.
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Spacecraft Power Bus Simulator
AMETEK Programmable Power, Inc.
*Provides enhanced measurement and data-logging of up to 40 channels.*Bus Power Monitoring Unit (BPMU) can be easily relocated to TVAC chamber to ease cabling complications*Data can be viewed either in spreadsheet or graphical format*Spacecraft (Payload) Protection Unit (SPU) provides 10 μsec reaction to out-of-tolerance conditions g
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Solar Array Simulator
SAS
AMETEK Programmable Power, Inc.
A spacecraft solar array is subjected to large temperature excursions, varying insolation (the amount of sunlight falling on the array), mechanical changes and aging, which substantially effect both its short and long term performance. In order to test the spacecraft's power environment, a cost-effective solution for ground based testing is to utilize a solar array simulator.
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Thermal Testing
At E-Labs, Inc., we support thermal cycling and thermal bakeout vacuum testing requirements. During thermal cycling, the unit experiences repeated heating and cooling as it would when exposed to the harsh environment of space. During thermal bakeout, flight equipment is subjected to an outgassing reduction process so as to decrease the chance of molecular contamination of the spacecraft instrumentation.
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4 Channels, MIL-STD-1553, Dual Redundant, Transformer Coupled, Assisted Mode Capable (AMC)
FTC
MIL-STD-1553 is a military standard published by the United States Department of Defense that defines the mechanical, electrical, and functional characteristics of a serial data bus. It was originally designed for use with military avionics, but has also become commonly used in spacecraft On-Board-Data-Handling (OBDH) subsystems, both military and civil. It features a dual, redundant, balanced-line, physical layer; a (differential) network interface; time division multiplexing; half-duplex command/response protocol; and up to 31 remote terminals (devices).
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2 Channels, MIL-STD-1553, Dual Redundant, Transformer Coupled, Assisted Mode Capable (AMC)
FTB
MIL-STD-1553 is a military standard published by the United States Department of Defense that defines the mechanical, electrical, and functional characteristics of a serial data bus. It was originally designed for use with military avionics, but has also become commonly used in spacecraft On-Board-Data-Handling (OBDH) subsystems, both military and civil. It features a dual, redundant, balanced-line, physical layer; a (differential) network interface; time division multiplexing; half-duplex command/response protocol; and up to 31 remote terminals (devices).
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4 Channels, MIL-STD-1553, Dual Redundant, Direct Coupled, Assisted Mode Capable (AMC)
FTF
MIL-STD-1553 is a military standard published by the United States Department of Defense that defines the mechanical, electrical, and functional characteristics of a serial data bus. It was originally designed for use with military avionics, but has also become commonly used in spacecraft On-Board-Data-Handling (OBDH) subsystems, both military and civil. It features a dual, redundant, balanced-line, physical layer; a (differential) network interface; time division multiplexing; half-duplex command/response protocol; and up to 31 remote terminals (devices).
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1 Channel, MIL-STD-1553, Dual Redundant, Direct Coupled, Assisted Mode Capable (AMC)
FTD
MIL-STD-1553 is a military standard published by the United States Department of Defense that defines the mechanical, electrical, and functional characteristics of a serial data bus. It was originally designed for use with military avionics, but has also become commonly used in spacecraft On-Board-Data-Handling (OBDH) subsystems, both military and civil. It features a dual, redundant, balanced-line, physical layer; a (differential) network interface; time division multiplexing; half-duplex command/response protocol; and up to 31 remote terminals (devices).
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2 Channels, MIL-STD-1553, Dual Redundant, Direct Coupled, Assisted Mode Capable (AMC)
FTE
MIL-STD-1553 is a military standard published by the United States Department of Defense that defines the mechanical, electrical, and functional characteristics of a serial data bus. It was originally designed for use with military avionics, but has also become commonly used in spacecraft On-Board-Data-Handling (OBDH) subsystems, both military and civil. It features a dual, redundant, balanced-line, physical layer; a (differential) network interface; time division multiplexing; half-duplex command/response protocol; and up to 31 remote terminals (devices).
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1 Channel, MIL-STD-1553, Dual Redundant, Transformer Coupled, Assisted Mode Capable (AMC)
FTA
MIL-STD-1553 is a military standard published by the United States Department of Defense that defines the mechanical, electrical, and functional characteristics of a serial data bus. It was originally designed for use with military avionics, but has also become commonly used in spacecraft On-Board-Data-Handling (OBDH) subsystems, both military and civil. It features a dual, redundant, balanced-line, physical layer; a (differential) network interface; time division multiplexing; half-duplex command/response protocol; and up to 31 remote terminals (devices).
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16-Bit Logic
Redundancy of mission critical subsystems is a common practice used to ensure reliable operation of a spacecraft or satellite.
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Power Management ICs (PMICs)
Telecommunications and defense industries demand ever-increasing functionality in equipment such as satellites, probes and spacecrafts. CAES offers a family of radiation hardened Power Management Integrated Circuits (PMICs) designed for high reliability applications.
