PW-Sat

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PW-Sat is a series of Polish CubeSats designed and built by students at the Warsaw University of Technology in conjunction with the Faculty of Power and Aeronautical Engineering of Warsaw University of Technology, the Space Research Centre of Polish Academy of Sciences, and the European Space Agency. As of January 1, 2024, there have been 2 PW-Sats with a third in development. The first PW-Sat was the first Polish artificial satellite [1] which was launched 13 February 2012 from ELA-1 at Guiana Space Centre aboard Italian-built Vega launch vehicle during its maiden voyage. [2] After their graduation, the team that developed the original PW-Sat have also worked to develop the subsequent missions, establishing a private company named PW-Sat to design and manufacturer the PW-Sats, all of which test novel deorbiting methods, with the overall goal of the program to develop solutions to space debris. [3] [2]

Contents

PW-Sat1

PW-Sat
PW-Sat-testy-CBK.jpg
PW-Sat was the first Polish-built satellite.
Mission typeTechnology
Operator Polish Academy of Sciences (Space Research Centre)
COSPAR ID 2012-006G OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 38083
Mission duration1 year
Spacecraft properties
Spacecraft type1U CubeSat
Manufacturer Warsaw University of Technology (Faculty of Power and Aeronautical Engineering)
Launch mass1 kilogram (2.2 lb)
Start of mission
Launch date13 February 2012, 10:00:00 (2012-02-13UTC10Z) UTC
Rocket Vega VV01
Launch site Kourou ELV
Contractor Arianespace
End of mission
Decay date28 October 2014
Orbital parameters
Reference system Geocentric
Regime Low Earth
Perigee altitude 300 kilometres (190 mi)
Apogee altitude 1,023 kilometres (636 mi)
Inclination 69.47 degrees
Period 97.83 minutes
Epoch 9 November 2013, 01:40:17 UTC [4]
 

Development

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:

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-Sat2

PW-Sat2
PW-Sat2 Integrated PR-5.jpg
PW-Sat2 After its completion on 28 February 2018
Mission typeTechnology
COSPAR ID 2012-006G OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 38083 OOjs UI icon edit-ltr-progressive.svg
Spacecraft properties
Spacecraft type2U CubeSat
Manufacturer Warsaw University of Technology (Faculty of Power and Aeronautical Engineering)
Start of mission
Launch dateDecember 3, 2018
Rocket Falcon 9 v1.1 FT
Launch site Vandenberg Air Force Base SLC-4E
ContractorInnovative Space Logistics B.V. [12]
End of mission
Last contactSeptember 22, 2019
Decay dateFebruary 23, 2021
Orbital parameters
Reference system Geocentric
Regime Low Earth
PW-Sat2-logo.png
PW-Sat2 mission patch  

Development

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]

Mission

PW-Sat2 would be launched aboard the Falcon 9 SSO-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]

Hardware

Besides the aforementioned butane thruster, the 3U CubeSat will also carry the following hardware:

Mission

See also

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References

  1. 1 2 "PW-Sat, Poland's first satellite launched into orbit". 14 February 2012. Archived from the original on 3 October 2012. Retrieved 7 May 2012.
  2. 1 2 3 4 5 "AMSAT-UK | A voluntary organisation that supports the design and building of equipment for Amateur Radio Satellites". 22 February 2013. Archived from the original on 23 February 2013. Retrieved 7 May 2012.
  3. "about us". pw-sat.pl. Retrieved 12 January 2024.
  4. Peat, Chris (9 November 2013). "PW SAT - Orbit". Heavens Above. Retrieved 9 November 2013.
  5. "PW-Sat 1". Gunter's Space Page.
  6. 1 2 "Home". pw-sat.pl.
  7. Kanawka, Krzysztof. "Status misji PW-Sat (październik 2012)". kosmonauta.net (in Polish). Archived from the original on 13 October 2012.
  8. Kanawka, Krzysztof (17 September 2023). "Vega i PW-Sat - rok po starcie)". kosmonauta.net (in Polish).
  9. "Satelita" (in Polish). 2 January 2019.
  10. "PW-Sat2 gets 180 000 € to fund the launch". PW-Sat2: Polish student satellite project. Archived from the original on 31 January 2016. Retrieved 11 March 2016.
  11. 1 2 3 "PW-Sat2 (PWSat-2, PW-SAT2)". nanosats.eu. Retrieved 11 January 2024.
  12. "Oficjalne: PW-Sat 2 na Falcon 9!". Kosmonauta.net (in Polish). 17 September 2023.
  13. 1 2 3 4 5 6 "PW-Sat3". nanosats.eu. Retrieved 11 January 2024.