BRICSat-P

Last updated
BRICSat-P
Mission typeCommunications
Operator U.S. Navy [1]
COSPAR ID 2015-025E [1]
SATCAT no. 40655 [1]
Spacecraft properties
Bus 1.5U Cubesat
Manufacturer George Washington University
Launch mass1.9 kilograms (4.2 lb)
Dimensions10 by 10 by 15 centimetres (3.9 in × 3.9 in × 5.9 in)
Start of mission
Launch date20 May 2015, 15:05 UTC
Rocket Atlas V 501 AV-054
Launch site Cape Canaveral SLC-41
End of mission
DisposalDecommissioned
Orbital parameters
Reference system Geocentric
Regime Low Earth
Semi-major axis 6,772 kilometres (4,208 mi) [2]
Eccentricity 0.109060 [2]
Perigee altitude 327.8 kilometres (203.7 mi) [2]
Apogee altitude 475.5 kilometres (295.5 mi) [2]
Inclination 54.9773° [2]
Period 92.4 minutes [2]
RAAN 320.0527° [2]
Argument of perigee 152.7277° [2]
Mean motion 15.5764196 [2]
Epoch 26 June 2018 [2]
Transponders
Band FM
 

BRICSat-P or OSCAR 83 (NO-83) previously known as PSat-B, is a U.S. technology demonstration satellite and an amateur radio satellite for Packet Radio. BRICSat-P (Ballistic Reinforced Communication Satellite) is a low cost 1.5U CubeSat built by the U.S. Naval Academy Satellite Lab in collaboration with George Washington University, that will demonstrate on-orbit operation of a Micro-Cathode Arc Thruster (μCAT) electric propulsion system and carries an amateur communication payload.

Contents

Mission

A four μCAT thruster head system was placed on one side of the spacecraft around the center of gravity and will de-tumble the satellite from its initial expulsion, demonstrate rotational control about 2 axes, and perform a delta-V end of life scenario. Orbital analyses performed indicate that the four thruster-head system is able to fit in a 1.5U Cubesat with low power consumption such that other subsystems such as communication systems can perform normally. Dynamics analysis has been performed in MATLAB Simulink and STK that shows the thrusters can successfully perform the attitude control maneuvers. The project is fully funded and launched on 20 May 2015. [1]

Status

BRICSat-P suffered from power budget problems and has been unable to support all of its primary missions. [3]

Frequencies

BRICSat has 2 amateur communication payload on boards: APRS constellation transponder with downlink on 437.975 MHz and with uplink on 145.825 MHz 1k2 and 9k6 AX25 PSK31 transponder with a 28.120 MHz uplink (2.5 kHz bandwidth) and a UHF FM downlink. [4]

See also

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References

  1. 1 2 3 4 "BRICSat-P". NSSDCA. NASA GSFC. Retrieved 2018-06-26.PD-icon.svg This article incorporates text from this source, which is in the public domain.
  2. 1 2 3 4 5 6 7 8 9 10 "BRICSAT-P (NO-83)". n2yo.com. Retrieved 2018-06-26.
  3. Krebs, Gunter D. "BRICSat-P (BRICSat 1 / NO 83 / Naval Academy-OSCAR 83)". Gunter's Space Page. Retrieved December 11, 2022.
  4. "Communication and Data Handling System for BRICsat Satellite" (PDF). Tomáš Urbanec, Petr Vágner, Miroslav Kasal, Ondřej Baran (Brno University of Technology). Retrieved 2018-06-26.