The PÄYLOAD-2.0

Overview:
Size: 1/4-U (100x100x25 mm)
Components: CorePCB, AMU, S-band antenna
Antenna: 8 dBi gain, LHC polarized, 2.45 GHz
Purpose: Technology demonstrator, in-orbit validation, radiation measurement
Project Description
As part of the SOURCE-2 mission of KSat e.V. and the Institute of Space Systems at the University of Stuttgart (IRS), SeeSat e.V. is developing a payload for the in-orbit validation of new technologies: The PÄYLOAD-2.0. This includes a specially manufactured S-band antenna, the central computing unit of the ERWIN mission and experiments on newly developed software algorithms and the measurement of radiation effects in low earth orbit. The aim of the mission is to test and validate application-oriented technologies under real space conditions.
A central component of the payload is the CorePCB, a powerful computing unit based on the Xilinx Ultrascale+ MP-SoC platform, which will serve as a standardized computing platform for future SeeSat e.V. missions. The in-orbit validation tests the power supply, memory architecture and high-speed interfaces under real conditions.
Another key component is the S-band antennadeveloped by SeeSat e.V. itself and manufactured in cooperation with partner companies, which acts as the communication backbone of the payloads within the SOURCE-2 mission. The antenna will be certified according to the relevant ECSS standards as part of the cooperation, which represents an important step towards creating a reliable and cost-effective communication solution for student space missions.
In addition, an algorithm developed by the German Aerospace Center (DLR) is being tested that detects and corrects single event effects (SEEs) in memories in real time. Together with the investigation of beam effects on individual bits in dynamic and static memories, a scientifically sound “minimum spec” for error-correcting procedures (e.g. CRC) can be designed for future missions.
In addition, an Ambient Monitoring Unit (AMU) records the radiation dose and carries out differentiated gamma spectroscopy in order to document the radiation conditions in the Low Earth Orbit more precisely. This data is used to better assess the need for radiation-hard components and to develop economically viable solutions for future space missions.
The knowledge gained can be used to make sound design decisions for hardware and software in the future and further improve the reliability of space systems. In particular, the certification of the S-band antenna according to ECSS standards could provide SeeSat e.V. with space flight heritage for the first time and thus offer a solid, cost-efficient alternative to commercial solutions for other student space clubs.
Timeline
Phase 0: April 2024 - December 2024
Mission Analysis and Needs Identification
Phase A: January 2025 - July 2025
Preliminary Requirement Definition, Rough System Architecutre
Phase B: August 2025 - March 2026
Preliminary Design, Detailed System Architecture
Phase C: April 2026 - December 2026
Detailed Requirement Definition, First Engineering Model
Phase D: January 2027 - October 2027
Qualification and Testing Process, Flight Model, Integration into Satellite
Phase E: From launch
Radiation Measurement, S-Band Communication, In-Orbit-Validation
Phase F: 2030
Disposal




Team

Max Julius Bode
Project coordination, IOV Power

Marian Keller
AMU

Stefan Wertheimer
IOV Memory

Pascal Fiedler
IOV Memory

Hannah Feiler
S-band antenna