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ERM PRODUCTS
ERM Selection
Guide
ERM Concept
ERM Applications
E500
Specification
E1000
Specification
E2000
Specification
E4000
Specification
Load Feedback
Customer List
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The
ERM is a derivative of the BE2K Ejector (See
Custom Actuators).
The principal of operation is that a bolt is threaded into the coupler
section of the Actuator and used to secure a
spacecraft deployable. On
command the coupler section is released by powering the
Actuator.
The ERM is a uniquely simple and effective device which offers the following key
features:

High Load Capacity
The range of ERMs currently available have load capability of between 500
and
4000 lbs.
 Simple
Mounting
The ERM mounts to the structure via a two-point mounting flange and connects
to the deployable via a single bolt threaded into the coupler.

Fast Function Time
The ERM
can jettison the deployable with a standard pyro pulse limited to 5 amperes
and 50 milliseconds.

Simple Reset
The ERM can be reset
within seconds while still attached to the structure via a simple tool
provided by TiNi Aerospace.

High Life Cycle
The ERM has a minimum
life of 50 cycles.
 Redundant
Firing Circuit
As with all TiNi
Actuators a redundant SMA circuit is incorporated. This provides complete
electrical redundancy as well as mechanical redundancy for the critical TiNi
trigger element.

Auto Shut-Off Switches
Auto Shut
Off Switches are incorporated making each ERM operational using a wide range
of power levels.

Misalignment Protection
The ERM
has a swivel capability in which the Actuator
housing can rotate up to ±5 degrees within the mounting enclosure. This
is an important feature for applications where the deployable is hinged and
therefore traverses an arc as it is released.

Custom Configurations
As with
all TiNi Actuators custom configurations are readily attainable with minimum
effort.
 Detailed Specification
See spec sheet for each model or contact TiNi Aerospace. |

©2005 TiNi Aerospace, Inc.
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