LituanicaSAT-2

Last updated

LituanicaSAT-2
Operator Vilnius University, NanoAvionics
COSPAR ID 2017-036D OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 42768 OOjs UI icon edit-ltr-progressive.svg
Website n-avionics.com/lituanicasat-2/
Mission duration3-15 months (planned)
Start of mission
Launch date23 June 2017
Rocket PSLV
Launch site Sriharikota
Orbital parameters
Reference system Geocentric
Regime Low Earth
 

LituanicaSAT-2 is a 3U Lithuanian CubeSat satellite launched on a Polar Satellite Launch Vehicle. [1] This mission is led by Vilnius University in cooperation with NanoAvionics and is a part of the international "QB50" mission. LituanicaSAT-2 is an in-orbit technology demonstration mission during which the propulsion system prototype for small satellites will be tested. The satellite was deployed in Sun-synchronous orbit at an altitude of 475 km. [2]

Contents

"QB50" mission

LituanicaSAT-2 is a part of a network of 50 nano-satellites called "QB50" (EU 7FP project) led by Von Karman Institute, Belgium. [3] The science objective of the mission is to carry out long term measurements of key parameters and constituents in yet largely unexplored lower thermosphere and ionosphere. [4] The "QB50" mission is intended to demonstrate the possibility of launching a network of 50 CubeSats built by Universities Teams all over the world as a primary payload on a low-cost launch vehicle to perform first-class science. [5] Another purposes of the QB50 project is to achieve a sustained and affordable access to space for small scale research space missions and planetary exploration. [5]

The scientific purpose of LituanicaSAT-2 mission as a part of "QB50" is to provide long-term multipoint, in-situ measurements. The contribution of the LituanicaSAT-2 is to accomplish the molecular Oxygen measurements Flux-Φ-Probe Experiment (FIPEX). [2]

LituanicaSAT-2 mission objectives

LituanicaSAT-2 technical overview

Propulsion system prototype for small satellites used in LituanicaSAT-2. Propulsion system prototype.jpg
Propulsion system prototype for small satellites used in LituanicaSAT-2.

LituanicaSAT-2 is consisting of three main modules: a science unit with the FIPEX (Flux-Φ-Probe Experiment) sensor for "QB50", a functional unit with NanoAvionics Command and Service module plus power unit and an experimental unit with the "green" propulsion system. [4]

LituanicaSAT-2 is commanded by NanoAvionics SatBus 3C1 which is a main system bus unit based on high-performance, low power consumption STM ARM Cortex 32 bit architecture that integrates 3 in 1 functionality on a single board. [2]

LituanicaSAT-2 structural frame. Structural 2.jpg
LituanicaSAT-2 structural frame.

The propulsion sub-system is designed to provide 0.3N thrust and up to 200 m/s of delta V. The fuel used is a contemporary green monopropellant fuel blend based on ammonium dinitramide (ADN). It gives 252 s of Isp, has a density of 1.24 g/cm3 with a chamber temperature of 1600 °C. Key fuel selection factors were non-toxicity, stability and benign handling properties at the same time giving very similar or even better performance as a worldwide proven hydrazine monopropellants. Current TRL is at level 5/6. [3]

The power generation of LituanicaSAT-2 is provided by 4 fixed and 4 deployable mono crystalline silicon solar panels custom designed and manufactured by NanoAvionics. The panels are able to reach an efficiency of 20%. [2]

LituanicaSAT-2 structure is custom designed by NanoAvionics and manufactured locally. The structure is made of 7075 aluminium alloy with hard anodized surfaces. [2] Some of LituanicaSAT-2 parts were 3D-printed using special materials approved for aerospace industry. [6]

Launch

On 23 June 2017, the satellite was launched into Sun-synchronous orbit via PSLV. The propulsion tests were successfully executed on 5 July. [7]

See also

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References

  1. "NanoAvionics Preparing For LituanicaSAT-2 Launch In April". www.startuplithuania.lt. Retrieved 4 April 2017.
  2. 1 2 3 4 5 "LituanicaSAT-2 | NanoAvionics". n-avionics.com. Retrieved 4 September 2016.
  3. 1 2 3 4 "LituanicaSAT-2 – University Space Engineering Consortium". unisec-europe.eu. Retrieved 4 September 2016.
  4. 1 2 3 "LituanicaSAT 2 (QB50 LT01)". space.skyrocket.de. Retrieved 4 September 2016.
  5. 1 2 "THE PROJECT". www.qb50.eu. Archived from the original on 3 April 2015. Retrieved 4 September 2016.
  6. "LituanicaSAT-2 Parts". dukubu.lt. Retrieved 4 September 2016.
  7. Adamowski, Jaroslaw (8 August 2017). "Lithuanian nano-spacecraft industry player obtains 3.2M euros to commercialize propulsion system, performs successful in-orbit test". Spacenews. Retrieved 12 December 2018.