STP-H10 (original) (raw)
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STP-H10 [STP]
The STP-H10 (Space Test Program - Houston 10) is a combo of experiments to be hosted on the International Space Station (ISS).
STP-H10 consists of seven DoD SERB and NASA experiments integrated on the single platform:
- SPADE-3 (Space Plasma Diagnostic Suite) to Demonstrate rapid impedance data acquisition and evaluate surface mounted sensor performance
- Falcon ODIN (Falcon Optical Defense and Intelligence through Neuromorphics) to design, develop, and test a novel means of detecting lightning and transient luminous using a neuromorphic camera.
- TERI (cadmium zinc TElluride Radiation Imager) - The objective of the experiment is to space qualify imaging large crystal CZT detector technology and associated front end electronics.
- SPARTA (Space-Based Payload for Army Research Test-Bed Applications) is a weather radar capable of providing upper atmosphere weather data in a timely fashion for relevant DoD missions.
- NERDI-1B (Neutron Radiation Detection Instrument -1B) is to characterize the on-orbit performance of microstructured semiconductor neutron detectors with low-cost commercial electronics for use in a space-radiation environment.
- SFXTI (Solar Flare X-Ray Timing Investigation) is an investigation to reveal intricate morphology of solar flare acceleration at high spectral resolution and at unprecedented spatiotemporal scales.
- SEED (Space Edge Experiments and Demonstrations) - SEED is a developing edge-intelligent low SWaP payload capable of processing high resolution imagery on a reconfigurable basis for adaptive detection and/or classification of multiple areas and features of interest.
The STP-H10 package was launched as an external payload on the Dragon CRS-32 cargo spacecraft and is to be mounted on the Columbus Module COL-SOX site.
| Nation: | USA |
|---|---|
| Type / Application: | Technology |
| Operator: | US Space Force (USSF), STP (Space Test Program) |
| Contractors: | Aegis Aerospace |
| Equipment: | see above |
| Configuration: | Attached ISS payload |
| Propulsion: | None |
| Power: | Via ISS |
| Lifetime: | |
| Mass: | |
| Orbit: | 400 km × 400 km, 51.6� (typical) |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks |
|---|---|---|---|---|---|
| STP-H10 | N/A | 21.04.2025 | CCK LC-39A | Falcon-9 v1.2 (Block 5) | with Dragon CRS-32, ACES |
Further ISS missions: ISS complex