STP-H10

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

Launch Sites:

  • CCK =   NASA John F. Kennedy Space Center, Cape Canaveral, Florida, USA   USA

References:

Cite this page: