
Microsecond Hot-Fire Transient Capture & Rocket Engine DAQ
Ingest tens of thousands of combustion chamber pressure transducers, turbopump vibration accelerometers, and cryogenic flow sensors up to 100kHz. Capture ignition pressure spikes, acoustic resonances, and LOX/LH2 chill-down transients across ISRO LPSC, IPRC Mahendragiri, and SpaceX McGregor test stands.

Designed for Mission-Critical Fidelity
1. ISRO LPSC / IPRC Mahendragiri HAT & Cryogenic Test Stand
High Altitude Test (HAT) facility vacuum ignition simulation for CE-7.5 and CE-20 cryogenic upper stage engines. Monitor LOX/LH2 chill-down, turbopump cold flow, and CUS integrated stage static firing in real time.

One telemetry platform from component cold-flow to pad static fire
ISRO LPSC & MAHENDARAGIRI
SPACEX MCGREGOR & STARBASE
PAD STATIC FIRE & HOPS

From Mahendragiri HAT Chambers to McGregor Test Stands. Zero Data Loss.
Rocket Propulsion Ground Testing & Validation Flow
Standard rocket engine & stage testing workflow using ISRO (LPSC / IPRC Mahendragiri) & SpaceX (McGregor Test Facility, Texas) industry terminology.
ISRO 1. Solid Motor Testing (SHAR STEX Complex)
Static Test and Evaluation Complex (STEX) firing at SDSC SHAR
Propellant grain burn rate & acoustic sub-scale motor validation
Segmented booster static test firing (S200 solid rocket booster)

Engineered for High-Fidelity Domain Telemetry
100 kHz Ingest Rate
Native C++ edge buffer handles extreme data bursts without backpressure.
Nanosecond Sync
PTP IEEE 1588 synchronization across distributed test stands.
Air-Gapped Security
Deploy on isolated local subnets with zero internet dependency.
LabVIEW & MATLAB Integration
Pre-built connectors for industry standard test bench software.
Parquet & HDF5 Export
Instant export into open columnar data formats for post-test analysis.
Real-time FFT Graphs
Sub-10ms web UI graph updates for vibration and acoustic signatures.
Proven Results in Mission-Critical Facilities
Engineers diagnose combustion instability in seconds rather than hours.
Zero data drop recorded during high vibration propulsion runs.
Fully reproducible telemetry sessions with immutable timestamps.
PILOT PROGRAM
Ready to transform your rocket engine hot-fire test stand?
Connect your test stand, vehicle fleet, or edge sensors in under 15 minutes with our native edge binaries.