
PADRE [University of California]
PADRE (solar PolArization and Directivity X-Ray Experiment) is NASA cubesat mission to study the Sun. The mission is a collaboration between the Space Sciences Laboratory University of California Berkeley (SSL/UCB), Goddard Space Flight Center (GSFC), SouthWest Research Institute (SWRI), University of Applied Sciences and Arts Northwestern Switzerland (FHNW), the Saclay Nuclear Research Centre of the Commissariat ā lénergie atomique (CEA-Saclay).
As a 12U solar spinner CubeSat, PADRE focuses on measuring the polarization and directivity of hard X-rays (HXRs) emitted during flares, unraveling the behaviors and distributions of high-energy electrons in the Suns atmosphere. Developed on a EnduroSat CubeSat platform, PADRE combines advanced instrumentation with a robust, cost-effective design.
Solar flares are the most powerful explosions in the solar system, yet there are many parts of their mechanisms that scientists dont fully understand. During a flare, the Sun releases magnetic energy violently and rapidly enough to accelerate charged particles to relativistic speeds. The details of the energy conversion process and particle propagation during this acceleration are largely unknown. PADREs mission will revolutionize our understanding of solar flare physics by determining the angular distribution of flare-accelerated electrons through the observation of two hard X-ray (HXR) characteristics:
HXRs are emitted by energetic electrons via bremsstrahlung collisions with ambient ions, making them the most direct available characteristic of solar flare electron acceleration. These observations will provide more thorough diagnostics for constraining different flare particle acceleration scenarios.
| Nation: | USA |
|---|---|
| Type / Application: | Astronomy, solar |
| Operator: | University of California, Berkeley for NASA |
| Contractors: | EnduroSat (bus), University of California, Berkeley (payload) |
| Equipment: | |
| Configuration: | CubeSat (12U) |
| Propulsion: | |
| Power: | 2 deployable fixed solar arrays, batteries |
| Lifetime: | |
| Mass: | |
| Orbit: |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| PADRE | 2025-135AH | 23.06.2025 | Va SLC-4E | Falcon-9 v1.2 (Block 5) | with Nyx Mission Possible, W-Series 4, VanZyl 2, Capella 17, T1DES 1, Arvaker 2, 3, SkyBee A02, Lyra 3, ICEYE X52, ..., X57, IRIDE-MS2-HEO 2, ..., 6, 8, 9, GHGSat C12, C13, Startical IOD-2, ForgeStar 1, GRUS 3α, BIFROST, ElaraSat MMS1, EarthDaily 1, Pulsar 0, ION-SCV 018, Lemur-2 TBD1, TBD2, ION-SCV 020, Otter Pup 2, Hubble 4, 5, Hubble 6, 7, PADRE, BRO 18, AddCube, AE2a, AE3Va, ARCSTONE, Connecta-IoT 9, ..., 12, DUTHSat 2, Hyperfield 1B, MÖBIUS 1, SATMAR, Sejong 2, FossaSat 2E21, JACK 001, PARUS T2, QUICKģ, SATORO T3, TPA 1, Time Flies, UND-ROADS 1, 2, Good Ancestor Kilakila, HORIS 1, 2, RIDUSAT, |
