LAUNCH VEHICLES
ROCKET & LAUNCH VEHICLE TESTING
EXPENDABLE LAUNCH VEHICLES (ELVs), REUSABLE LAUNCH VEHICLES (RLVs), HYBRID LAUNCH VEHICLES
Testing Challenges:
- Collecting physical measurements on rockets and launch vehicles, including force, vibration, shock, strain, and temperature
- Varied test scenarios: laboratory, sled, flight testing/in situ
- Harsh test environments, including wide temperature ranges
- Size, weight, and power constraints
- Complex, time-intensive test setups
- Short development cycles; limited access to test articles
- Long lead times on test instrumentation
DTS Key Features:
- SWaP-optimized (size, weight & power) data acquisition units
- Rapid deployment, embeds in the test article, no long cable runs
- High-shock rated, wide operating temps & environmental ratings
- Universal analog sensor support, built-in sensor options
- Onboard memory and real-time streaming (CH10, IENA or TmNS)
- Time synchronization via IEEE 1588 PTPv2
- Standalone, network, or integrate into an existing FTI solution
- COTS products; standard 4-6 week delivery
DTS ADVANCED MEASUREMENT SOLUTIONS - MINIATURE | RUGGED | HIGH-SPEED
RECOMMENDED DTS PRODUCTS FOR LAUNCH VEHICLE & ROCKET TESTING
SLICE6 AIR
SLICE6 AIR-BR
TSR AIR
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