PLX’s space heritage dates back to 1975 when the company provided hollow retroreflectors to the Apollo-Soyuz Russian-American space hookup program. The units were used in the docking procedure to align the two vehicles.
Ever since, PLX has been a part of some of the world’s most important space missions.
2018: ICESat-2 Launch.
For Ball Aerospace & Technologies Corporation PLX designed two LTHR’s™ for the Advanced Topographic Laser Altimeter System (ATLAS) program. ATLAS is the sole instrument on the ICESat-2 satellite.
The two LTHRs™ are part of the Alignment Monitoring and Control System. They are used to keep the laser and receiving telescope bore-sighted to each other during orbit.
2016: Canadian Astro-H Metrology System (CAMS) Program.
PLX Invar-mounted hard mount retroreflectors with 1.94” clear aperture and 0.5-arc second accuracy were provided to NEPTEC.These retroreflectors will be used to monitor the alignment of a 12 meter focal length x-ray telescope. CAMS is the metrology system designed to measure the lateral (X/Y) and rotational (roll) displacement in the spacecraft’s optical bench relative to the instruments.
ASTRO-H is expected to provide breakthrough results in scientific areas as diverse as the large-scale structure of the Universe and its evolution, the behavior of matter in the gravitational strong field regime, the physical conditions in sites of cosmic-ray acceleration, and the distribution of dark matter in galaxy clusters.
2016: Robotic Exploration of Mars.
The TIRVIM (Thermal Infra-Red V-Shape Interferometer Mounting) Spectrometer is part of the Atmospheric Chemistry Suite (ACS), launched in March 2016 and is now successfully operating in orbit around Mars.
Its scientific goal is to monitor temperature profiles and measure aerosol content during nadir observations.
The PLX Retroreflectors used in the TIRVIM Interferometer offer properties, which enable it to survive launch conditions and to perform in harsh environments while maintaining exceptional stability and accuracy.
2015: ICE, Cloud, and Land Elevation Project (ICESat-2).
PLX has supplied SGT a vacuum-compatible Lateral Transfer Hollow Retroreflector with a 5” aperture, 18.5” separation and 1 arc second accuracy. This unit is part of the ground support equipment for testing and verifying the Advanced Topographic Laser Altimeter System (ATLAS).
2009: Keldysh (Russian Federal Space Program).
This is a space application where the retros will undergo sinusoidal modulation in the range of 10-100 Hz. These retroreflectors are part of a device intended for remote sensing of the surface and atmosphere of Earth for hydrometeorological purposes. Data from this device is used for obtaining temperature/humidity profiles and trace gases monitoring, as well as for weather forecasting and prediction of climatic changes. This device will be launched integral with the “Meteor-M” satellite by the Russian Federal Space Program. Meteor-M represents a series of satellites with launch dates of 9/2009, 7/2014, 2015, 2016.
2005: ESA European Space Agency Venus Express.
Another PFS (Planetary Fourier Spectrometer) unit, also containing PLX retroreflectors, has been launched by ESA as part of the “Venus Express.” The goal of this program is to perform a global investigation of the Venusian atmosphere.
2003: Optical Units for the European Space Agency Mars Express launch.
The PFS is an instrument developed by the European Space Agency (ESA) to study the atmosphere and soil of Mars. The main optical units of the PFS are not Michelson Interferometers, but rotating interferometers containing the PLX retroreflectors. This instrument is much less sensitive to mechanical disturbances than conventional Michelson interferometers. PFS was launched from the Baikonur Cosmodrome in Kazakhstan in June 2003 as part of the Mars Express. The main objective of the Mars Express is to search for sub-surface water from orbit and to drop a lander on the Martian surface.
Another PFS was launched by ESA in November 2005 aboard the Venus Express. The goal of this program is to perform a global investigation of the Venusian atmosphere.
2003: Canadian Space Agency SCISAT-1 atmospheric experiment.
ACE-FTS Atmospheric Chemistry Experiment Fourier Transform Spectrometer, built by ABB Bomem in conjunction with the Canadian Space Agency. PLX retroreflectors provide modulation in the ACE-FTS which is a Michelson interferometer.
Launched aboard SCISAT-1. The major goal of this experiment is to measure and understand the chemical processes that control the distribution of ozone in the Earth’s atmosphere. The ACE-FTS instrument simultaneously measures the temperature, trace gases, thin clouds and aerosols in the atmosphere.
2002: NASA’s Earth Science Enterprise EOS-CHEM spacecraft.
PLX provided beryllium assemblies for the Thermal Emission Spectrometer (TES) built by Jet Propulsion Laboratory for NASA. TES is a high-resolution infrared imaging FTIR spectrometer designed to measure the state of the Earth’s troposphere.
Other PLX-designed instruments chosen for TES included back-to-back Hollow Retroreflector™ assemblies, Hollow Roof Mirror™ assemblies and various folding mirrors, all made of beryllium. With accuracies that were better than 1 arc second maximum deviation and λ/20 surface flatness (λ=633nm), these instruments operated without distortion at cryogenic temperatures down to –100°C after surviving launch vibration conditions.
2000: NASA’s Endeavor Shuttle Radar Mission.
PLX designed a Retroreflector Array™ for creating a high-resolution digital topographic database of the Earth.
JPL deployed corner reflectors during the mission. These are highly reflective structures that appear as a bright point in the radar image. These reflectors deployed with precisely measured coordinates, served as control points in the Shuttle Radar Topography Mission data.
1997: Retroreflector In Space (RIS) for NASDA, the Japanese Space Agency.
PLX designed and manufactured the 50cm (20”) diameter Retroreflector In Space (RIS) for NASDA, the Japanese Space Agency. The largest retroreflector ever sent into space
RIS achieved 1 second of arc accuracy and contained a curved mirror to compensate for the movement of the satellite through space. RIS (Retroreflector In Space) is a retroreflector for an earth-satellite-earth laser used in long-path absorption experiments. RIS has a corner-cube structure with an effective diameter of 50 cm. Measurements of ozone, CFC12, CO2, CH4, etc. are carried out using infrared pulsed lasers.
1990: Relay Mirror Experiment – NASA with Ball Aerospace.
The Relay Mirror Experiment (RME) successfully demonstrated long-range, low-jitter tracking and pointing capabilities appropriate for ground-based laser (GBL) propagation. Relay mirrors have been proposed as a method of increasing the range of laser weapons that is less costly than deploying a larger number of laser weapons.
1990: LACE Experiment – NASA.
Low-power Atmospheric Compensation (LACE) was an experiment paired with RME.
1985: Discovery Shuttle Long Distance Laser test.
PLX also built retroreflector components for NASA’s Discovery Shuttle Long-Distance Laser Test performed in 1985. This used an 8 inch Retroreflector mounted to one of Discovery’s windows.
A low power laser was launched from Maui. The test was a part of the SDIO “Star Wars” program and was intended to see if it was possible to target and track a high flying fast moving object. It also was to determine the effects of atmospheric aberrations on the laser beam.
1975: Apollo-Soyuz Russian/American 1975 Space Union – NASA.
In the 1970’s PLX provided Hollow Retroreflectors™ to the Apollo-Soyuz Russian-American space hookup program. The units were used to measure gases in the environment of the vehicles.