Thrust Testing Services
Element helps you validate rocket propulsion systems faster and with less risk. Our advanced thrust testing capabilities combine static fire testing, multi-axis thrust measurement up to 50,000 lbf, and cryogenic propulsion support, backed by 50+ years of propulsion test heritage to accelerate your aerospace and defense development programs.
What is Thrust Testing at Element?
Thrust testing evaluates the performance, force output, and structural behavior of rocket propulsion systems under operational conditions. These tests help validate propulsion performance, system reliability, and qualification readiness for aerospace and defense applications.
At Element, thrust testing combines static fire testing, multi-axis force measurement, cryogenic fluid handling, and high-pressure propulsion infrastructure to support rocket engine development, qualification, and performance validation programs.
What Can Element Offer You For Thrust Testing?
Key tests offered
Key tests offered
Element performs rocket propulsion thrust testing, static fire testing, multi-axis force measurement, high-pressure fluid testing, and cryogenic propulsion support to validate propulsion system performance under operational and extreme conditions.
- Static rocket engine testing
- Multi-axis thrust measurement
- Hot-fire testing
- Propulsion performance characterization
- High-pressure fluid testing
- Cryogenic propulsion testing
Cutting-edge equipment we use
Cutting-edge equipment we use
Element's San Bernardino facility includes two rocket testing platforms designed for 20,000 lbf thrust engines, integrated cooling systems for extremely hot exhaust gases, NOx mitigation systems, and a dedicated water-cooled exhaust duct system.
The rocket test stand thrust measuring system (TMS) supports:
- Multi-axis force measurement
- Up to 50,000 lbf single-axis thrust measurement
- 8,000 lbf side/asymmetric load measurement
- Remote load cell calibration capabilities
Methods and solutions offered
Methods and solutions offered
Element supports propulsion development and qualification programs from early-stage testing through performance validation and certification support. Integrated propulsion testing capabilities combine thrust measurement, cryogenic fluid systems, high-temperature testing, and advanced data acquisition to simulate real-world operational environments.
Components and materials we test
Components and materials we test
Element tests rocket engines, propulsion systems, fuel and propellant systems, pressurized assemblies, valves, piping systems, and high-pressure aerospace components used in aerospace and defense applications.
Materials and media handled include:
- Hydrogen
- Oxygen
- Nitrogen
- Methane
- Carbon dioxide
- High-pressure steam and water systems
Which Element Labs offer this service
Which Element Labs offer this service
Thrust testing is delivered from Element's San Bernardino, California facility, a dedicated 50+ year aerospace propulsion development test site, A2LA-accredited (Cert. 0214.45), and operating in full compliance with ASME, API, and South Coast Air Quality Management District requirements.
Standards we test to and Components we test
Aerospace & Defense Standards
- MIL-STD-1474
- MIL-STD-740-1
- MIL-STD-740-2
- MIL-STD-810 (environmental simulation – relevant subsections)
- DO-160 (relevant subsections for propulsion electronics)
Pressure & Piping Standards
- ASME B31.3
- ASME Boiler & Pressure Vessel Code
- API Piping Codes
- ASME B31.1 (Power Piping)
Accreditation & Quality
- ISO/IEC 17025 (A2LA Cert. 0214.45)
Rocket Propulsion Systems
- Rocket engines
- Propulsion systems
- Static fire assemblies
- Fuel and propellant systems
High-Pressure Systems
- Pressure vessels
- Cryogenic systems
- Pressurized assemblies
- Valves and fittings
- High-pressure piping systems
Your Challenges, Our Solutions
Validate propulsion performance
Reduce propulsion risk
Handle extreme environments
Streamline qualification testing
Why Choose Element
Advanced thrust measurement
Integrated propulsion expertise
Specialized test infrastructure
Aerospace testing experience
50,000 lbf Single-axis thrust measurement capability
20,000 lbf Rocket testing platform design capacity
4,475 psig ASME-coded blow-down tank capacity at 700 °F
50+ years Rocket propulsion testing experience
Frequently asked questions
What is the difference between static fire testing and hot-fire testing?
Static fire testing holds a propulsion system stationary while firing it at full thrust to measure axial force, ignition transients, and shutdown behavior. Hot-fire testing is a broader term covering any test in which a propulsion system runs at operational temperatures and pressures – it includes static fire but also longer-duration performance characterization and qualification runs.
Can Element support both liquid and cryogenic propulsion systems?
Yes. Element's San Bernardino facility handles cryogenic media including liquid hydrogen, liquid oxygen, methane, and nitrogen, with temperature capability down to -452 °F, and supports both pressure-fed and pump-fed liquid propulsion systems.
What thrust range can Element measure?
Up to 50,000 lbf single-axis, with 8,000 lbf side/asymmetric load measurement for multi-axis configurations. Two rocket testing platforms are designed for 20,000 lbf-class engines.
Is Element's propulsion lab accredited?
Yes. Element San Bernardino holds A2LA accreditation (Certificate 0214.45) to ISO/IEC 17025 for environmental, mechanical, and high-pressure fluid testing of aerospace components, and operates to ASME and API piping codes.
Can you accommodate customer-supplied test articles and bespoke test plans?
Yes. Element supports customer-defined test profiles, witnessed testing, video and high-speed data capture, and remote viewing where required by program security or scheduling.
Global expertise
Working with Element, you have access to our global network of materials testing and product qualification test experts. Meet our Engaged Experts.
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