Additional space-rated-solution capabilities are described below.

They are low shock and highly reliable for use in launch vehicles, satellites, and payload systems. Misalignment Protection –  All ERMs have a swivel feature such that the Actuator can rotate +/-5 degrees within its mounting enclosure. Disconnects for deadfaced, EVA, high voltage, in flight, and vertical-launch applications. Connector separation is assisted by an ejector spring. We'll assume you're ok with this, but you can opt-out if you wish. Contributing to a sustainable future; Health and safety; COVID-19 Update; Environment; People ; Ethics and business conduct; Careers.

These have to be light-weight, efficient and highly reliable. Cryogenic applications including fuel monitoring. It is also an excellent text for upper-level undergraduate and graduate-level courses in astronautical and mechanical engineering. Job search; Investors. Standard ERM reset tools come in two basic designs – A bottle opener style with folding arms and a basic jackscrew type that is turned using a “T” handle or torque wrench via a hex head. Copyright © 2020 Ensign-Bickford Aerospace & Defense Company. jfair@ced.us.com A center-screw thread facilitates mating and demating. Low-imparted-shock, positive mate monitoring, and zero-separation-force connectors. CED provides mission critical devices for launch vehicles such as Atlas V and Delta IV, space exploration vehicles such as Mars Rover, and satellites such as MUOS and Galileo. You also have the option to opt-out of these cookies. Chemring’s separation bolts are designed and manufactured for use in applications where rapid structure separation is demanded. Power configurations based on MIL-DTL-5015 inserts in shell sizes 25L to 37. Additional features include: Visit the MIL-DTL-38999 NATC space-rated connectors page for more information. Business Segment Manager, Life Support Programs This makes them very “user friendly” and operable from a wide range of current and voltages.

Anti-bind roll-off shells, 360-degree EMI protection, electrically and thermally deadfaced configurations, push-pull snap action couplings, and visual and tactile mating indicators. In some cases, customers require custom reset tools to accommodate space constraints. Necessary cookies are absolutely essential for the website to function properly.

The table below provides a list of reset tools for each of our standard ERMs. This Standard specifies the requirements applicable to the concept definition, design, analysis, development, production, test verification and in­orbit operation of space mechanisms on spacecraft and payloads in order to meet the mission performance requirements.

This is an important feature which protects against binding due to possible misalignment, and or instances where the deployable traverses an arc after release (such as in hinged assemblies). Auto Shut-Off Switches – Simple Auto Shut Off Switches are incorporated into each ERM to protect the TiNi™ Trigger. The 6-32 size attaching screw can be preloaded into the coupler to generate 250 lbf (1112 N) of preload. Chemring is a leading space component supplier, with a 55-year heritage proven through key space programs. This category only includes cookies that ensures basic functionalities and security features of the website.

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Chemring’s separation nuts are designed and manufactured for use in applications where rapid structure separation is demanded. The ERM is simple to use and easy to reset and offers the same key attributes as all of our legacy products including: The EBAD TiNi™ E2000 ERM (Ejector Release Mechanism) is an effective way to support and release spacecraft deployables.

NEA (Non-Explosive Actuators) – As with all EBAD TiNi™ products, the ERM is non-pyrotechnic and field reset-able with a minimum qualified life of 50 cycles. The ERM is simple to use and easy to reset and offers the same key attributes as all of our legacy products including: The EBAD TiNi™ standard ERM is rated for a minimum life of 50 actuation and reset cycles. Custom capabilities include thermal and electrical deadfaces and special insert patterns and shell configurations. Redundant Firing Circuit – As with all TiNi™ Actuators a redundant SMA circuit is incorporated. It is mandatory to procure user consent prior to running these cookies on your website.

Eaton's custom-solutions capabilities enable quick-turn development of cost-effective and reliable space-rated solutions that are reusable, serviceable, and upgradeable. NATC connectors, low-imparted-shock solutions, and custom-cable assemblies. (Please use the tabs below to see different product options). Fast Acting – All TiNi™ ERMs can be actuated with a standard pyro pulse of only 25 milliseconds or less.

Since 1987, our space technologies group has flown thousands of mechanisms on hundreds of space missions.

Design options include: Eaton's Space and Launch Capabilities brochure provides heritage-proven-solution information for applications ranging from launch pads to mission payloads: Use the link below to register for PDF or printed copies; due to export-controls restrictions, this brochure is not downloadable from this web site. Cell bypass switches for battery and solar-panel applications. The PC-23 initiator is the commercial equivalent to the NASA Standard Initiator for non-NASA customers than can used on space missions. The ERM is simple to use and easy to reset and offers the same key attributes as all of our legacy products including: The EBAD TiNi™ E1000 ERM (Ejector Release Mechanism) is an effective way to support and release spacecraft deployables. The EBAD TiNi™ Ejector Release Mechanism (ERM) is a uniquely simple and effective device which offers both high load holding capability and fast actuation time. The cutters are designed for robustness and can be used in space as well as in deep submergence applications. Near simultaneous release of multiple hold-down points.

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Standard products and engineered-to-order solutions are available to meet a wide range of application-specific requirements: The depicted solution incorporates three isolated insert compartments for flight, ordinance, and instrumentation contact groups and is qualified for use on the Peacekeeper Missile.

Scope. Deployable solar panels have been widely used for the generation of enough power in CubeSats due to their limited volume area for solar cell integration.

Space Vehicle Mechanisms is an indispensable resource for engineers involved in the design and analysis of mechanical assemblies used in space flight, and a valuable reference for space systems engineers, mission planners, and control systems engineers. On 3 June we announced our interim results.

The ERM is simple to use and easy to reset and offers the same key attributes as all of our legacy products including: Specification subject to revision. Custom configurations available under request. We also use third-party cookies that help us analyze and understand how you use this website. But opting out of some of these cookies may have an effect on your browsing experience.

The EBAD TiNi™ E500 ERM (Ejector Release Mechanism) is an effective way to support and release spacecraft deployables. Copyright © document.write(new Date().getFullYear()) Eaton, Non-Explosive Actuators & Release Mechanisms, Privacy, cookies and data protection policy, Responsible sourcing of conflict minerals.

Fully integrated connector-and-actuator solutions in mechanically and electrically initiated configurations. Flight Qualified – The ERM is a derivative of the EBAD TiNi™ Pinpuller product line and was first flight qualified in March of 2001.

A resettable release mechanism was developed based on a separation-nut design with over 40 years of flight heritage. They are low shock and highly reliable for use in launch vehicles, satellites, and payload systems. Fully European technology. Air, Space & Defence markets are looking for more and more Mechatronic Solutions for improving flight or observation performance.. To discuss your application-specific requirements, call 805-484-0543 or e-mail cicustomer.service@eaton.com For continued testing, EBAD™ provides reset tools of various shapes and designs. Space launch initiators and release mechanisms; Aircraft safety components; Missile and electronics; Explosive materials; Breaching and demolition; Pyro-mechanisms; Extruded Double Base (EDB) Propellants; Publications; Sustainability. The EBAD TiNi™ E500 ERM (Ejector Release Mechanism) is an effective way to support and release spacecraft deployables. Umbilical solutions, interstage-separation connectors, and rack and panel configurations. Space-qualified parts and materials.

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ITAR/EAR free. Chemring’s thrusters have been long used in many types of launch vehicles. NASA SSQ 21635 NATC Available in 53 standard contact patterns including bussed configurations.

A lanyard mechanical release is initiated by missile-stage separation.

The 10-32 size attaching screw can be preloaded into the coupler to generate 1000 lbf (4448 N) of preload.