UNSW-EC0 (QB50-AU02)
Australia
Spacecraft nº:
Australian spacecraft nº: 20
Part of the QB50 constellation.
Launch data:
Designation
42723 / 98067MC
Launch date
18 Apr 2017
Launch site
CC, SLC-41
Launch vehicle
Atlas V-401
Mission
Space Science, thermospheric research
Launch platform
ISS Kibo, LEO
Deployment date
25 May 2017 - 05:25 UT
Earth orbit:
Perigee / Apogee
400 x 404 km
Inclination
51.6°
Period
92.4 min
Launched together with:
Cygnus CRS-7
-
ALTAIR 1
-
SUSAT
-
i-INSPIRE 2
-
ZA-AeroSat
-
nSIGHT 1
-
Ex-Alta 1
-
LilacSat 1
-
NJUST 1
-
Aoxiang 1
-
SOMP 2
-
QBITO
-
Aalto 2
-
X-CubeSat
-
SpaceCube
-
DUTHSat
-
UPSat
-
Hoopoe
-
LINK
-
SNUSAT 1 & 1b
-
qbee50-LTU-OC
-
BeEagleSat
-
HAVELSAT
-
Phoenix
-
PolylTAN-2-SAU
-
QBUS 1, 2 & 4
-
IceCube
-
CSUNSat 1
-
CXBN 2
-
KySat 3
-
SHARC
-
Biarri-Point
-
Lemur-2 30-33
Spacecraft data:
Prime manufacturer
University of New South Wales
Platform
2U cubesat
Operator
University of New South Wales
Mass at launch
2 kg
Dry Mass
kg
Basic shape
Dimension (m)
Equipment
Solar array
Solar cells
Stabilization
Propulsion
None
DC power
Uplink (MHz)
Downlink (MHz)
437.510
Beacon (MHz)
Mode
9600bps MSK
Call sign
QBUS01
Status
Active
End of live:
Re-entered date:
03 Dec 2018 (.64)
Lifetime:
Description:
USNW-EC0 is a 2U QB50-AU02, from the University of New South Wales in Sydney.
It carries the INMS (Ion/Neutral Mass Spectrometer), which measures the mass of ions and neutral atoms, as the primary payload for the QB50 project.
The satellite also carries four non-QB50 Payloads:
the Namuru GPS Board
the seL4bit SBC seL4 microkernel board to carry out critical functions (ADC)
the RUSH FPGA, a radiation tolerant FPGA SBC to provide user defined downtime in case of SEU, capable of “no loss of service”
RAMSES, a 3D printed Satellite Structure using Selective Laser Sintering of high temperature thermoplastic
Ref.
: #3(SD554), #7(JR738), #14, #228 - update: 25.08.19
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