Adcole Space (Redwire)

Manufacturer United States Verified
17 Products
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About Adcole Space (Redwire)

Adcole Space, now operating as part of Redwire Corporation following its acquisition, is a US-based manufacturer of space-grade sun sensors and optical attitude determination products with over 60 years of heritage on hundreds of orbital missions. Headquartered in Jacksonville, Florida (Redwire), Adcole Space produces digital sun sensors, analog sun sensors, and coarse sun sensors for spacecraft attitude determination, with flight heritage spanning NASA, ESA, and commercial missions including the Orion spacecraft on NASA's Artemis II mission. Redwire's broader space portfolio encompasses advanced solar arrays, spacecraft platforms, on-orbit servicing technologies, and space-based defence systems serving government and commercial customers.

Products

17

A single-detector analog sun sensor using the cosine principle for solar array pointing, sun acquisition, and fail-safe recovery. Over 1,000 units deployed since the 1960s across hundreds of spacecraft.

1 8

A two-axis analog sun sensor assembly containing four cosine-response detectors in a pyramid arrangement for full-hemisphere sun detection. Used for solar array pointing, sun acquisition, and fail-safe recovery.

2 8

A two-axis digital sun sensor with ±32° field of view offering higher accuracy than the ±64° variant. Radiation-hardened to 100 krad (Si) with Hi-Rel components for GEO and deep-space missions.

2 7

A two-axis digital sun sensor with ±64° field of view providing medium-accuracy attitude determination. Up to 8 optical heads per electronics unit with proven deep-space flight heritage on Mars 2020 and Parker Solar Probe.

2 9

A high-accuracy spinning spacecraft sun sensor with redundant optical heads and electronics delivering better performance than the Miniature variant, for sun acquisition and attitude determination.

1 7

A high-precision sun sensor for attitude control applications requiring sub-arcminute accuracy and millidegree angular resolution. Available in single or dual-axis configurations and fully customizable.

2 7

The dynamic simulator provides a HITL (Hardware In The Loop) test set for the MAI-400 which verifies and validates all software and hardware functions in a bench top setting. In…

1 2

This 1/2U Attitude and Determination and Control System features 3 reaction wheels, a 3-axis magnetometer, a 2-camera Earth Horizon Sensor (EHS), 3 torque rods and an ADACS…

1

The MAI400 Controller Board incorporates four microcontrollers with a 3-axis MEMS accelerometer, 3-axis MEMS gyroscope and 3 sets of Reaction Wheel and Electromagnet drive…

1 2

The MAI-400 reaction wheels are offered as a complete, standalone reaction wheel assembly unit for CubeSats and NanoSat missions. The motor driver electronics, which includes an…

1 2

The MAI KE Sun Sensor can be used for a variety of spacecraft missions requiring sun detection. The output of the MAI KE sun Sensor is an analog voltage that ranges from…

1 2

The MAI-SES is a miniature Static Earth Sensor suitable for CubeSats, NanoSats, and larger spacecraft in Low Earth Orbit. It is designed to be mounted inside a MAI-400 unit but…

1 2

The MAI-SS Star Tracker is low in cost and intended for CubeSat and NanoSat missions. The unit is completely self-contained and features lost in space star identification. Just…

1 1

A compact sun sensor for spinning spacecraft providing sun aspect angle and sun crossing pulses for spin rate and spin axis orientation determination, with ±87.5° FOV and 0.25 kg mass.

1 8

A miniature autonomous star tracker for CubeSat and NanoSat missions delivering 10 arcsecond quaternion accuracy at 4 Hz update rate, weighing only 475 grams with Lost-in-Space star identification.

1 13

Ground support equipment that generates a simulated star field for functional testing and verification of the SpectraTRAC and other Adcole Space star trackers during spacecraft integration and test.

1 4

Ground support equipment using infrared LEDs to optically stimulate Adcole sun sensor cells for functional verification, aliveness testing, and flight harness checkout during spacecraft integration.

1 6

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