NELS

- Non-Explosive Low Shock (NELS) hold-down and release system

STATUS | Completed
STATUS DATE | 09/10/2018
ACTIVITY CODE | 4E.045

Objectives

© Airbus Defence and Space NL

The first phase of the development covered requirements definition, technology investigation, bread-board testing and concept design. A trade-off was made between the concepts designs, and decisions were made on the concept used for the Engineering Model. 

Key elements in the design were to increase the pre-load capability, lower the shock induced with the actual release, and ensure a wider operating temperature range. At the same time increase the flexible positioning tolerances and keep a compact and structure that is able to cope with the high mechanical loads.

For the design we have chosen to use a Thermal Knife cutting technology in combination with a VECTRAN cable for the release of the system. The VECTRAN cable offers a high preload capability of 15kN typical load and above 50kN break load.

This model was subjected to a series of tests. The result of the tests were reviewed with ESA

Challenges

Main challenges have been to find the material for the cable and[A1]  come up with a design for the cutting mechanism that is compatible with that cable and fits in a design that meets the project requirements. In particular finding the material for the cable and how that can be cut in a controlled manner has been the key objective during the development. After that making a design for the Hold Down that can handle the higher loads.

System Architecture

Increased demands from the S/C applications, including satisfying higher margins of safety requires a re-design of the existing ARA mk3 design. The need for higher pre-tension systems from S/C conditions (in certain failure modes) and requiring a larger temperature range than can be met with the ARA mk3 design.

Therefore the NELS development has the approach to extend the pre-tension to 15kN with a design that that has a high level of similarity with the existing ARA mk3 design, and to increase the temperature envelope.

Plan

In summary the project covered the following steps: 

  • Requirements consolidation
  • Complete the conceptual design
  • Preliminary design of the EM model and the related tooling and test set-up.
  • BB and subsequently EM testing of the Thermal Knives.
  • Develop an Alternative for the Thermal Knives
  • Restraint cable development testing
  • Restraint cable EM testing
  • Build the EM NELS, tooling and test set-up
  • EM Functional testing
  • System characterisation, including pre-load testing, humidity test, random vibration, APTC and repetitive cutting tests
  • Test reporting

Current Status

All activities in the ARTES 5.2 project are completed, with the exception of testing a 2nd run of the Thermal Knives and its assembly; ready to progress to formal qualification under a ARTES 3-4 project .