The PW-Sat project was created in 2004 when group of students from Warsaw University of Technology decided to build satellite compatible with CubeSat 1U standard.[1] Initially planned for a 2007 launch, delays in the development of the Vega caused the mission to be postponed until 2012.[citation needed] The cost of the project was estimated to be 200,000 Polish zloty (63,205 USD), with funding coming from the university's budget, as well as from an agreement between Poland and the European Space Agency.[citation needed]
Hardware
PW-Sat1 was a 10x10x10 cm cube with a mass of 1 kg. It is equipped with the following hardware:
CW beacon transmitting on 145.901 MHz for tracking by radio amateurs
Mission
PW-Sat1 was launched on 13 February 2012, 10:00 UTC from ELA-1 at Guiana Space Centre (Kourou, French Guiana) aboard the maiden flight of the Vega rocket, together with LARES and ALMASat-1 satellites and 6 other CubeSats built by various European universities.[2][5] It was deployed 1 hour 10 minutes into the flight from the P-POD-2 container, along with the ROBUSTA and MaSat-1 CubeSats.[6]
First signals from satellite were received around 12:10 UTC by radio amateurs.[2] The first Polish reception of PW-Sat1's signals came at 12:15 UTC by CAMK in Warsaw.[6]
PW-Sat1 was planned stay in orbit until 2013, when it was planned to perform a destructive atmospheric reentry.[2] The satellite used a large amount of the batteries' stored energy while performing tasks early in the mission. This battery depletion, combined with orbital maneuvers designed so the satellite would fly over Poland, delayed deployment of the tail. Commands of tail deployment were sent from Earth on April and May 2012, but PW-Sat did not respond to the commands.[7] Due to a hardware issue with the communication module (that was discovered on a few other CubeSats using the same model) communication with the satellite was problematic and the tail couldn't be extended.[8]
PW-Sat1 reentered the atmosphere on 28 October 2014.[9]
Development of a successor, PW-Sat2, begun in September 2013 and was launched in December 2018.[10][11]
PW-Sat1's successor, PW-Sat2 was also developed by students at the Warsaw University of Technology immediately after the launch of PW-Sat1. The cubesat's primary payload was a 2m by 2m solar sail technology demonstration, meant to de orbit PW-Sat2 as a proof of concept for the technology. However, PW-Sat2 would only deploy its sail after a 40-day window so that its secondary payload, an experimental sun sensor, can perform its tests.[11]
Hardware
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Mission
PW-Sat2 would be launched aboard the Falcon 9SSO-A's SERPA flight on December 3, 2018. The probe successfully deployed its secondary payload and after the allotted 40 day window deployed its primary payload. However, the solar sail would fail to deorbit PW-Sat2, and would instead begin to deteriorate. Although the exact cause of the sail's failure is not known, the PW-Sat2 team's "leading hypothesis is that temperature gradient between sail foil and arms leads to tension and breaking the foil." Regardless, PW-Sat2 deorbited along its original path on February 23, 2021, however, the last update from the team was on September 22, 2019.[11]
PW-Sat3
Development
A third cubesat, the PW-Sat3 is currently under development by students at the Warsaw University of Technology. This rendition of the satellite is expected for launch in 2024 aboard an RFA One on the launch vehicle's second ever launch. PW-Sat3 will be controlled by a KP Labs Antelope on-board computer running Oryx modular flight software.[13]
The PW-Sat3's mission requires a change in altitude and as such required the design of an onboard thruster. The cold gas thruster uses butane as a propellant and will perform station-keeping maneuvers and at the end of the mission will perform the deorbiting maneuver.[13]
The satellite's launch has been significantly delayed to no earlier than late 2025 due to delays in the development of the RFA One.
Hardware
Besides the aforementioned butane thruster, the 3U CubeSat will also carry the following hardware:
AOCS system: The primary payload, a custom AOCS system that will be used during propulsion maneuvers to align the satellite in the optimal orientation.[13]
EHS sensors: The secondary experiment, a series of Earth Horizon Sensors made from industrial IR matrixes.[13]
Camera module: Similarly to PW-Sat2, PW-Sat3 will have an onboard camera to document the probe and its experiments.[13]
The development team is planning on having an onboard transponder that would allow amateur radio enthusiasts to broadcast radio packets and to possibly download on-demand low-resolution images from the camera. After the completion of its scientific payloads, PW-Sat3's radio will emit a series of commemorative radio beacons before final deorbiting. The development team has also promised that all telemetry frame formats will be thoroughly described and made publicly available on the project website, as well as decoders and the accompanying software application.[13]
Mission
This section is empty. You can help by adding to it. (January 2024)
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
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