Telemetry in the context of "Telematic control unit"

The refresh rate, also known as vertical refresh rate, vertical scan rate or vertical frequency in reference to terminology originating with cathode-ray tubes (CRTs), is the number of times per second that a raster-based display device displays a new image. This is independent from frame rate, which describes how many images are stored or generated every second by the device driving the display. On CRT displays, higher refresh rates produce less flickering, thereby reducing eye strain. In other technologies such as liquid-crystal displays, the refresh rate affects only how often the image can potentially be updated.

Non-raster displays may not have a characteristic refresh rate. Vector displays, for instance, do not trace the entire screen, only the actual lines comprising the displayed image, so refresh speed may differ by the size and complexity of the image data. For computer programs or telemetry, the term is sometimes applied to how frequently a datum is updated with a new external value from another source (for example; a shared public spreadsheet or hardware feed).

A ground segment consists of all the ground-based elements of a space system used by operators and support personnel, as opposed to the space segment and user segment. The ground segment enables management of a spacecraft, and distribution of payload data and telemetry among interested parties on the ground. The primary elements of a ground segment are:

• Ground (or Earth) stations, which provide radio interfaces with spacecraft
• Mission control (or operations) centers, from which spacecraft are managed
• Remote terminals, used by support personnel
• Spacecraft integration and test facilities
• Launch facilities
• Ground networks, which allow for communication between the other ground elements

These elements are present in nearly all space missions, whether commercial, military, or scientific. They may be located together or separated geographically, and they may be operated by different parties. Some elements may support multiple spacecraft simultaneously.

A stream gauge, streamgage or stream gauging station is a location used by hydrologists or environmental scientists to monitor and test terrestrial bodies of water. Hydrometric measurements of water level surface elevation ("stage") and/or volumetric discharge (flow) are generally taken and observations of biota and water quality may also be made. The locations of gauging stations are often found on topographical maps. Some gauging stations are highly automated and may include telemetry capability transmitted to a central data logging facility.

A GPS tracking unit, commonly referred to as a GPS tracker or simply tracker, is a device used as part of a tracking system to track the location of the asset it is connected to. It uses a Global Navigation Satellite System (GNSS) to determine its geographic position. This location data, along with other vehicle or asset telemetry, is transmitted to an Internet-connected device or a central server using an embedded cellular, radio, or satellite modem. This enables the real-time monitoring and management of vehicles, assets, personnel, and animals from a remote location, and is used in intelligent transportation systems. The global market was valued at over $2.5 billion in 2022 and projected to grow at a CAGR of over 13% to reach $4.76 billion by 2027.

GPS tracking units are used by consumers and are a component of fleet telematics systems and fleet digitalization. Data collected by these devices is typically sent to specialized fleet management software platforms. While many modern vehicles are equipped with a factory-installed telematic control unit (TCU) from the manufacturer, aftermarket GPS tracking units are used to manage mixed fleets (with vehicles from different brands) and to equip vehicles that lack native telematics systems. Specialized hardware manufacturers produce these devices.

In navigation, a radio beacon or radiobeacon is a kind of beacon, a device that marks a fixed location and allows direction-finding equipment to find relative bearing. It is a fixed-position radio transmitter which radiates radio waves which are received by navigation instruments on ships, aircraft or vehicles.

The beacon transmits a continuous or periodic radio signal on a specified radio frequency containing limited information (for example, its identification or location). Occasionally, the beacon's transmission includes other information, such as telemetric or meteorological data.

A primary (or portable or personal) life support system (or subsystem) (PLSS), is a device connected to an astronaut or cosmonaut's spacesuit, which allows extra-vehicular activity (EVA) with maximum freedom, independent of a spacecraft's life support system. A PLSS is generally worn like a backpack. The functions performed by the PLSS include:

• Regulating suit pressure
• Providing breathable oxygen
• Removing carbon dioxide, humidity, odors, and contaminants from breathing oxygen
• Cooling and recirculating oxygen through the pressure garment, and water through a Liquid Cooling and Ventilation Garment or Liquid Cooling Garment.
• Two-way voice communication
• Display or telemetry of suit health parameters
• Telemetry of an indicator of the wearer's immediate health (e.g. heart rate)

The air handling function of a PLSS is similar to that of a diving rebreather, in that exhaled gases are recycled into the breathing gas in a closed loop.

Sputnik 2 (Russian pronunciation: [ˈsputʲnʲɪk], Russian: Спутник-2, Satellite 2), or Prosteyshiy Sputnik 2 (PS-2, Russian: Простейший Спутник 2, Simplest Satellite 2), launched on 3 November 1957, was the second spacecraft launched into Earth orbit, and the first to carry an animal into orbit, a Soviet space dog named Laika.

Launched by the Soviet Union via a modified R-7 intercontinental ballistic missile, Sputnik 2 was a 4-metre-high (13 ft) cone-shaped capsule with a base diameter of 2 metres (6.6 ft) that weighed around 500 kilograms (1,100 lb), though it was not designed to separate from the rocket core that brought it to orbit, bringing the total mass in orbit to 7.79 tonnes (17,200 lb). It contained several compartments for radio transmitters, a telemetry system, a programming unit, a regeneration and temperature-control system for the cabin, and scientific instruments. A separate sealed cabin contained the dog Laika.

A launch pad is an above-ground facility from which a rocket-powered missile or space vehicle is vertically launched. The term launch pad can be used to describe just the central launch platform (mobile launcher platform), or the entire complex (launch complex). The entire complex will include a launch mount or launch platform to physically support the vehicle, a service structure with umbilicals, and the infrastructure required to provide propellants, cryogenic fluids, electrical power, communications, telemetry, rocket assembly, payload processing, storage facilities for propellants and gases, equipment, access roads, and drainage.

Most launch pads include fixed service structures to provide one or more access platforms to assemble, inspect, and maintain the vehicle and to allow access to the spacecraft, including the loading of crew. The pad may contain a flame deflection structure to prevent the intense heat of the rocket exhaust from damaging the vehicle or pad structures, and a sound suppression system spraying large quantities of water may be employed. The pad may also be protected by lightning arresters. A spaceport typically includes multiple launch complexes and other supporting infrastructure.

KickSat was a satellite dispenser for small-satellite (femtosatellite) project inaugurated in early October 2011, to launch many very small satellites from a 3U CubeSat. The satellites have been characterized as being the size of a large postage stamp.and also as "cracker size".The mission launch was originally scheduled for late 2013 and was launched April 18, 2014.

Kicksat reached its orbit and transmitted beacon signals that were received by radio amateurs. Telemetry data allowed the prediction of the orbit and the reentry on May 15, 2014, at about 01:30 UTC. Due to a non-redundant design, a timer reset while on-orbit and the femtosatellites were not deployed in time, and burned up inside the KickSat mothership when the undeployed satellite-deployment mechanism reentered Earth's atmosphere. It is one of several crowdfunded satellites launched during the 2010s.