Skip Navigation
SBIR/STTR

Lightweight Inflatable Structural Airlock (LISA), Phase I

Completed Technology Project

Project Introduction

Innovative light-weight airlock technologies are required to integrate with any deep space and surface platform hosting Extra-Vehicular Activity (EVA). The CFD Research Corporation (CFDRC) team proposes an inflatable airlock structure that employs unique fabric architecture capable of delivering the lowest mass and greatest versatility of any competing design. The proposed fabric inflatable airlock design features a completely integrated air beam inter-wall to passively generate the wall stiffness required for airlock depressurization—without the mass and bulk of aluminum pressure hulls or complexity of multi-structure adaptations of competing inflatable habitat architectures. The design is a modification of Thin Red Line Aerospace's (TRLA) patented Ultra High Performance Pressure Vessel (UHPV), the only fabric pressure vessel design with fully determinate load paths which allows for true mass optimization. This unique architecture utilizes a matrix of braided fiber tendons to contain the structure's global pressure loads. The underlying woven fabric and gas barrier envelopes are thereby only exposed to minimal local shell loads where they bulge outwards between adjacent tendons. Working in pure tension in the absence of load coupling, the tendon array architecture has been shown to be statically determinate and auto-stabilizing under extreme deflection. The proposed fabric inflatable airlock stows compactly for transport to the habitat further reducing logistic costs. More »

Anticipated Benefits

Primary U.S. Work Locations and Key Partners

Share this Project

Organizational Responsibility

Project Management

Project Duration

Technology Maturity (TRL)

Technology Areas

Light bulb

Suggest an Edit

Recommend changes and additions to this project record.
^