Blast Testing

Blast Testing

BLAST TESTING

Military Vehicles Feature Image - MRAP Testing - Photo Credit-USMC

MILITARY BLAST TESTING & VELOCITY OF DETONATION (VOD)

VEHICLE VALIDATION, STRUCTURAL INTEGRITY & SOLDIER SAFETY

Testing Challenges:

  • Dynamic, high-energy tests, often in remote locations
  • Measure the effect of blast waves on a wide range of test subjects, including vehicles, structures, and occupants
  • Occupant safety, accurate injury kinematics
  • Extensive time and monetary investment in test setup
  • Destruction of test article(s), which may include prototypes
  • Synchronization of high-speed cameras, triggers, power, and communication

DTS Key Features:

  • High-shock rated data acquisition systems and sensors
  • Miniature systems designed to embed on or in the test article
  • High data sampling rates, up to 1 million samples per second
  • Survivable up to 20,000 g, no special enclosures required
  • Accurate and reliable, data writes to non-volatile flash memory
  • Trusted solutions provider; experts in crash, blast, injury biomechanics testing

DID YOU KNOW? DTS manufactures the Warrior Injury Assessment Manikin (WIAMan) for the U.S. Army—the most biofidelic and technologically advanced test manikin ever developed for underbody blast and IED testing

DTS ADVANCED MEASUREMENT SOLUTIONS - MINIATURE | RUGGED | HIGH-SPEED

RECOMMENDED DTS PRODUCTS FOR BLAST TESTING

DTS SLICE HG Data Acquisition System Product Photo

SLICE HG

SLICE PRO Data Acquisition System

SLICE PRO

DTS SLICE6 AIR-BR Data Acquisition Unit

TSR 6DXP

DTS SLICE6 Data Acquisition System

SLICE MICRO

SLICE NANO Data Acquisition System

SLICE NANO

ATD-Vertical-Load-Blast

WIAMan

EV Crash Test Photo Credit IIHS

Corporate

Aircraft

Aircraft

AIRCRAFT

Aircraft - RASCAL Pods - Photo Courtesy of USAF - Christian Turner
Aircraft - eVTOL -Photo Courtesy of Volocopter

FIXED WING, AIRPLANE, ROTORCRAFT, HELICOPTER, & eVTOL FLIGHT TESTING

DYNAMIC IN-FLIGHT TESTING FOR ROTORCRAFT VEHICLES

Testing Challenges:

  • Collecting physical measurements on aircraft including force, vibration, shock, strain, and temperature
  • Varied test scenarios: laboratory, sled, flight testing/in situ
  • Harsh test environments
  • Remote locations with limited or restricted comm access
  • Size, mass, and power constraints
  • Complex, time-intensive test setups
  • Costly and noisy slip rings for rotating applications
  • Long leads and costs, especially for custom solutions

DTS Key Features:

  • SWaP-optimized (size, weight & power) data acquisition units 
  • Embeds in the test article near the sensors, no long cable runs
  • Significantly reduces or eliminates the need for slip rings
  • High-shock rated, IP68 rated solutions available
  • MIL-STD rated systems for temperature, altitude, shock & vibration
  • Wide range of analog sensor support, plus built-in sensor options
  • Onboard memory and real-time streaming options
  • 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 AIRCRAFT

DTS SLICE6 Data Acquisition System

SLICE6 AIR

DTS SLICE6 AIR-BR Data Acquisition Unit

SLICE6 AIR-BR

The DTS TSR AIR Data Logger

TSR AIR

SLICE NANO Data Acquisition System

SLICE NANO

DTS SLICE6 Data Acquisition System

SLICE MICRO

EV Crash Test Photo Credit IIHS

Corporate

Launch Vehicles

Launch Vehicles

LAUNCH VEHICLES

Launch Vehicles - SpaceX Starship Launch
Launch Vehicles - Photo Credit: NASA-Kim Shiflett
Launch Vehicles - Photo Credit: NASA-Kim Shiflett

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

DTS SLICE6 Data Acquisition System

SLICE6 AIR

DTS SLICE6 AIR-BR Data Acquisition Unit

SLICE6 AIR-BR

The DTS TSR AIR Data Logger

TSR AIR

EV Crash Test Photo Credit IIHS

Corporate

Hypersonic Vehicles

Hypersonic Vehicles

HYPERSONIC VEHICLES

Hypersonic Vehicle Application Main Photo - Photo Credit Sandia National Laboratories
Hypersonic Vehicle Sounding Rocket Photo Credit Sandia National Laboratories
Sandia Labs - Hypersonics Glide Body - Photo Courtesy of U.S. Navy

HYPERSONIC VEHICLE TESTING – SOUNDING ROCKETS & GLIDE VEHICLES

MEASURING LAUNCH FORCES, VIBRATION & TEMPERATURE ON HYPERSONIC VEHICLES  

Testing Challenges:

  • In situ testing of hypersonic glide and boost-glide vehicles (HGV), hypersonic cruise missiles, experimental aircraft, and sounding rockets
  • Collecting force, vibration, shock, strain, temperature, and more
  • 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
  • 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
  • Supports short-duration and sustained flight testing applications
  • COTS products; standard 4-6 week delivery
DTS ADVANCED MEASUREMENT SOLUTIONS - MINIATURE | RUGGED | HIGH-SPEED

RECOMMENDED DTS PRODUCTS FOR HYPERSONIC VEHICLE TESTING

DTS SLICE6 Data Acquisition System

SLICE6 AIR

Video & Images Courtesy of Sandia National Laboraties / Hypersonics Glide Body – Photo Courtesy of U.S. Navy

EV Crash Test Photo Credit IIHS

Corporate

Ordnance

Ordnance

ORDNANCE

MISSILE, FUZE, ORDNANCE, BUNKER BUSTER & HARD TARGET TESTING

RELIABILITY, SAFETY, AND PRECISION IN HIGH-SHOCK TEST ENVIRONMENTS

Testing Challenges:

  • Dynamic, high-energy test environments
  • Remote locations, limited access to test article
  • Strict size and mass constraints, no space for protective housing or large power supplies
  • Complications with trailing or external cabling
  • High-value assets, costly test setups
  • Reliability and security of data transmission

    DTS Key Features:

    • Miniature rugged data acquisition systems and sensors
    • High-shock rated systems up to 20,000 g, proven reliability
    • Designed to embed in the test article near sensors; small enough to fit into an artillery round
    • Data acquisition and data logger options with built-in sensors
    • Onboard memory, plus real-time streaming options
    • Trusted solution provider; experts in crash, blast, and injury biomechanics testing
    DTS ADVANCED MEASUREMENT SOLUTIONS - MINIATURE | RUGGED | HIGH-SPEED

    RECOMMENDED DTS PRODUCTS FOR ORDNANCE TESTING

    DTS SLICE6 Data Acquisition System

    SLICE6 AIR

    DTS SLICE6 AIR-BR Data Acquisition Unit

    SLICE6 AIR-BR

    DTS SLICE HG Data Acquisition System Product Photo

    SLICE HG

    SLICE NANO Data Acquisition System

    SLICE NANO

    DTS SLICE6 AIR-BR Data Acquisition Unit

    TSR 6DXP

    EV Crash Test Photo Credit IIHS

    Corporate

    Space Missions

    Space Missions

    SPACE MISSIONS

    NASA Orion with Test Dummies and DTS DAQ Photo Credit NASA
    NASA Orion drop test Photo Credit: NASA
    Mars Sample Return - Perseverance

    ASTRONAUT SAFETY, SPACE CAPSULE INTEGRITY & DROP TESTING

    NASA ORION SPACE CAPSULE, ARTEMIS MOON MISSIONS & MARS SAMPLE RETURN PROGRAM SUPPORT

    Testing Challenges:

    • Harsh test environments, including the moon!
    • Structural integrity, full-scale and high-altitude drop testing  
    • Crew safety testing with instrumented test manikins to measure launch and re-entry forces that astronauts may experience
    • Limited space and weight constraints 
    • Time-intensive and costly test setups 
    • Limited or no access to instrumentation; power considerations
    • Synchronization of high-speed cameras, triggers, power, communication, and data management

     

    DTS Key Features:

    • Miniature, rugged data acquisition systems and sensors
    • Modular, configurable onboard solutions to support hundreds of sensors, including strain gauges and accelerometers
    • Data loggers with built-in sensors; ideal for unattended monitoring
    • In-dummy DAS solutions for the full family of crash test 
    • Ancillary accessories to support power, trigger, & communication
    • Data writes to non-volatile flash memory, plus streaming options
    • Experts in crash safety & injury biomechanics testing
    DTS ADVANCED MEASUREMENT SOLUTIONS - MINIATURE | RUGGED | HIGH-SPEED

    RECOMMENDED DTS PRODUCTS FOR NASA SPACE MISSIONS

    DTS SLICE6 Data Acquisition System

    SLICE6 AIR

    DTS SLICE6 AIR-BR Data Acquisition Unit

    SLICE6 AIR-BR

    The DTS TSR AIR Data Logger

    TSR AIR

    DTS SLICE6 Data Acquisition System

    TSR PRO

    SLICE NANO Data Acquisition System

    SLICE NANO

    DTS SLICE6 Data Acquisition System

    SLICE MICRO

    EV Crash Test Photo Credit IIHS

    Corporate

    Egress & Ejection Safety

    Egress & Ejection Safety

    EGRESS & EJECTION SAFETY

    Ejection Seat Application Feature Image Thumbnail

    EGRESS & EJECTION SAFETY TESTING 

    FULL-SCALE TESTING FOR STRUCTURAL INTEGRITY, PERFORMANCE & PILOT SAFETY

    Testing Challenges:

    • High-shock test environments, extreme weather conditions
    • Size, mass, and power constraints
    • Collecting physical measurements force, moments, vibration, shock, strain, and injury criteria
    • Structural integrity and aerodynamics characterization
    • Varied test scenarios: ejection seats, rocket sled, parachutes, airlift delivery testing, cargo airdrops, and low-altitude parachute-extraction system (LAPES) deliveries

    DTS Key Features:

    • SWaP-optimized (size, weight & power) data acquisition units
    • Rugged, high-shock rated
    • Embeds in the test article near the sensors, no long cable runs
    • Modular, configurable, high sampling rates up to 1M sps
    • MIL-STD rated systems for temperature, altitude, shock & vibration
    • Wide range of analog sensor support, plus built-in sensor options
    • Onboard memory and real-time streaming options
    DTS ADVANCED MEASUREMENT SOLUTIONS - MINIATURE | RUGGED | HIGH-SPEED

    RECOMMENDED DTS PRODUCTS FOR EGRESS & EJECTION SAFETY TESTING

    SLICE NANO Data Acquisition System

    SLICE NANO

    DTS SLICE6 Data Acquisition System

    SLICE MICRO

    The DTS TSR AIR Data Logger

    TSR AIR

    SLICE PRO Data Acquisition System

    SLICE PRO

    EV Crash Test Photo Credit IIHS

    Corporate

    HELP CENTER