Assessing the Application Requirements

Your specific application is very important to us. Please consider the factors listed below, along with your application requirements. We offer many styles of cable and cable assemblies that can be utilized in Military and Commercial Applications.

Electrical Requirements: Physical Requirements:

Frequency
Power Rating (Peak and Average)
Insertion Loss
VSWR

The frequency, power rating, I.L. and VSWR are probably the paramount requirements in designing a cable assembly. These four requirements will probably define the cable type and the connectors to be used.

Electrical Length
Phase
Delay Time

Any requirements on electrical length, phase, or delay time of a cable assembly are directly affected by the cable velocity of propagation and the operating frequency. The engineering department at Astrolab can help you define these parameters.

Astrolab will also design and manufacture phase matched cable assemblies or delay lines to your specifications.

Limits on Signal Leakage and Interference

Any limits on signal leakage will effect the selection of cable regarding the cable shielding.

Astrolab is able to design and manufacture custom cable to your exact specifications.

 

Cable Assembly Length

Cable assembly length is defined as the distance between the reference planes or center lines of the connectors. See the “cable assembly length tolerance table” in this section for standard tolerances on lengths.

Astrolab can manufacture cable assemblies to tighter length tolerances.

Pre-Defined Cable Routing

This generally requires a semi-rigid cable that is bent to a pre-defined form or shape to fit the application. Astrolab can manufacture and form semi-rigid cable assemblies that meet exact customer requirements.

Pre-Defined Connector Type and Gender

On a system where ports are already defined, the connector type and gender are pre-determined. You, however, must determine whether a “straight” connector will suffice or if you need a “sweep” or “right angle” connector. The connector mounting (bulkhead, flange or none) should also be considered. Of course, you must verify that the selected connector will support the frequency and power requirements of the application. See the “connector selection guide” within this section.

Physical Size Limitations
Weight

Physical size limitations and weight are always factors when selecting cable and connectors. Space applications are especially sensitive to these requirements.

Flexing Conditions

The bend radius, flex angle, number of flexes, rate of flexure, distance from anchor point etc. all contribute to the selection of the appropriate cable for your flexing condition. Astrolab already has or can design a cable to meet your flexing requirement(s) from semi-rigid cables which are typically flexed only once to ever-flex®, which can flex up to 3,000,000 times.

 

Environmental Conditions:

Temperature Extremes
Altitude
Space Environment

Cable assemblies operating at extreme temperature, altitude or in a space environment will require special materials or special conditioning of the materials that are used in both the cable and the connectors. Pre-conditioning, thermal cycling and outgassing using Astrolab's established procedures allow cable assemblies to be used in these environments.

Humidity
Corrosive Environments

Abrasive Environments

If a cable assembly will be subjected to the elements, Astrolab offers three levels of ruggedization, from polyolefin sleeving (to protect against moisture and solar radiation) to armor ruggedization (with crush resistance up to 1,000 lbs/inch). For connector protection consider plating the connector to increase resistance to oxidation. Some applications may require a hermetic seal connector or an o-ring/gasket fitted flange or bulkhead.

Vibration
Radiation

Handling, transportation and end use determine the vibration and radiation levels that a cable assembly will be subjected to. Astrolab can provide a cable assembly for use in the seeker head of a missile mounted on the wing tip of a high performance fighter jet, or that must survive the initial shock of a launch and the continuous mechanical stress, intense UV and gamma ray bombardment on a orbiting satellite.

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