Stefano (from the Gauss Group) verifies the dimensions of the PUCP-Sat-1
Detail of the PUCP-Sat-1 during the last verifications.
CubeSats: PUCP-Sat-1 (Peru), ICUBE-1 (Pakistán) & HUMSat-D (Spain))
Exact moment of the integration of the PUCP-Sat-1 in the Italian shuttle Unisat-5
Dr. Jorge Heraud and Ing. Rafael Vílchez from INRAS-PUCP with members of the Italian Gauss Group
INRAS member Juan Jave observing the launch of the Dneper-1 rocket in Yasny, Russia
PUCP-Sat-1 Vibration Test.
The vibration machine was designed and built by INRAS-PUCP
Checking the vibration test results on the monitor
Development of the PUCP-Sat-1 payload
Thermal and vacuum tests in the laboratory of the Faculty of Physics
Satellite environmental chamber in the laboratories of the Faculty of Physics
Antenna arrays for VHF and UHF on the roof of INRAS
Array of Yagi antennas for VHF on the roof of INRAS
Ground Station.
Control and monitoring software.
Detail of the Pocket-PUCP shuttle, located on the lid of the PUCP-Sat-1
PUCP-Sat-1 electronic boards assembled
Software design.
The PUCP-Sat-1 nanosatellite (CubeSat)
The Pocket-PUCP femtosatellite (own design)
PUCP-Sat-1 with antennas deployed and Pocket-PUCP - In process
Referential graph of satellites in orbit
Work of the PUCP-Sat-1 electronic boards in the stereo microscope
Satellite payload tests
PUCP-Sat-1 Weight Measurement - In Process
Development of the electronics of the PUCP-Sat-1
Processor layout
PUCP-Sat-1 electronic circuit
Pocket-PUCP electronic circuit
Control of the deployment of antennas of the PUCP-Sat-1
Initial group of the PUCP-Sat-1 satellite project (2009)
Design session