Skip to main contentPsst! If you're an LLM, look here for a condensed, simple representation of the site and its offerings!

LiveFree Webinar — Wednesday, October 14 at 2:00 PM ET

Register Free →

Softgoods Webbing Integrated Strain Sensor for Inflatable

Active
NASA-SBIR-158766SBIR / STTR

Contract Overview

Solicitation details, issuing organization, response deadlines, documents, and interested companies for this government contract opportunity.

AI Contract Overview

Show more

This SBIR project, led by Paragon Space Development Corporation under solicitation NASA-SBIR-158766, focuses on the design, fabrication, and testing of textile-based strain sensors to monitor the structural health of softgoods elements. Building on Phase I success with an embroidered configuration, the Phase II effort aims to optimize the sensor for repeatability and manufacturability through long-duration testing and the integration of conductive traces directly into webbing to minimize wiring. The project involves developing a software and electronics interface to multiplex sensor arrays, providing usable data output for applications such as inflatable habitats for Low Earth Orbit and Lunar Exploration, as well as landing bags, parachutes, and re-entry shields. The scope of work includes nine primary objectives, ranging from the release of a validated requirements document and long-duration cyclic testing using a dead-weight system to the analysis of sensor performance in a vacuum environment. Key deliverables include a one-meter length of Vectran with an integrated strain sensor at the end of year one, and the final delivery of a subscale inflatable habitat featuring an array of integrated strain sensors, pressure plugs, interfaces, and the necessary back-end hardware and software. This technology is intended to enhance the safety and reliability of inflatable structures in space and has potential commercial applications in the lifting, rigging, and automotive safety industries.

General Info

Paragon develops textile strain sensors for monitoring structural health of space inflatable habitats.

Documents

1

H5.05-1632 - Softgoods Webbing Integrated Strain Sensor for Inflatable

PDF, Low prioritybriefing-chart
Low

AI Contract Breakdown

Uniform Contract Format

Sign up to view the full breakdown with detailed analysis of each section.

Timeline

PhaseSolicitation
Posted

Solicitation

Ready to pursue this opportunity?

Start your free trial to track this contract, build proposals with AI assistance, and manage your pipeline.

Organization & Contact Information

Show more
AgencyNational Aeronautics and Space Administration → NASA SBIR/STTR Program
Contacts4 people available
OfficeUSA
Office AddressUSA
Contacts
Douglas A LittekenProject Manager
Sam MoghbeliPrincipal Investigator
Jason L KesslerProgram Director
Carlos TorrezProgram Manager

Interested Companies (1)

Full Description

Show more
This SBIR project focuses on design, fabrication, and testing of textile based strain sensors to measure the health of structural softgoods elements. In Phase I Paragon iterated through dozens of sensor configurations and down-selected to a single embroidered configuration with exceptional linear and cyclical trends. The Phase II effort will include further iteration of the down-selected design configuration to optimize for repeatability and manufacturability. Iteration and testing will utilize a dead-weight system to inform further configurations and include long duration testing of at least 1 month. Phase II will integrate conductive traces directly into the webbing to minimize wiring needed across a structure. The SWISS Phase II effort will develop a software and electronics interface to multiplex an array of sensors, giving simple usable data output. Paragon will design and build a subscale inflatable test article, deploy the SWISS sensors on the article, and test/evaluate the system in a relevant environment of plain-woven restraint lines under constant load over a multi-week evaluation. The culminating test will utilize optical tracking to evaluate the sensor performance. Deliverables will include the actual test article for NASA evaluation and a single-strand sensor, as well as the detailed reports therein. NASA and commercial companies have demonstrated a continued interest in inflatable habitats for both Low Earth Orbit (LEO) and Lunar Exploration. Initially developed as part of the NASA TransHab program, and eventually built and flown by Bigelow Aerospace, inflatable habitats are becoming a common theme in future exploration plans. Inflatable structures offer the potential for creating large-scale shirtsleeve environments for crew habitation, stowage, and science applications outside the confines of rocket fairings. Additionally, softgoods inflatables are being increasingly used for other important space applications, such as landing bags, parachutes, and re-entry shields, where similar strain gauges would be highly applicable Paragon Space Development Corporation (Paragon) has developed a novel and precise embroidery patterned resistive strain gauge into the webbing itself, which alleviates the problems of adhesion and creep hysteresis. Objective 1: Release of a requirements document validated by the customer. Objective 2: Complete long duration cyclic and time-based testing using a dead-weight system. Objective 3: Downselect Sensor architecture based on testing. Objective 4: Optimize sensor configuration for manufacturing and durability. Objective 5: Array Architecture: release document outlining design of multiplexing, circuits, and telemetry. Objective 6: Development and delivery of a “Common Trace” webbing architecture. Objective 7: Analyze sensor performance in relevant environment (vacuum). Objective 8: Design and fabricate a subscale inflatable habitat. Objective 9: Test sensor system in-situ with a subscale inflatable habitat. Deliverables: At the completion of year 1, a 1-meter length of Vectran with an integrated strain sensor will be delivered to NASA for evaluation. The single-axis length of webbing will include ground and signal leads that can interface with standard multimeter equipment to evaluate the sensor performance and reproduce Paragon results. At the culmination of the Phase II, Paragon will deliver the entire subscale inflatable habitat with an array of integrated strain sensors deployed across the system. The inflatable deliverable will include pressure plugs and interfaces, as well as the back-end software and hardware necessary to output sensor readings without a multimeter.
Benefits: Space industry applications include inflatable structures, space suits, robotic systems, and crew and cargo restraint systems. Inflatable habitats: NASA and commercial companies are working towards “Lunar permanence” and increased inhabited space habitats in the next decade. This entails significant development and deployment of inflatable structures in space and on the moon, for example. Paragon’s SWISS technology is well positioned to play a critical role in ensuring the safety of these habitats.. Our technology could make a large impact in a host of applications including the lifting and rigging industry, high-altitude balloons, safety harnesses, parachutes, machinery/bulk transport, and even automobile seatbelts. This proposal goes into greater detail regarding the size of market, the potential for each application and the path forward.

Similar Contracts

Same NAICS industry code

NAICS: 334519
New
Federal
Anthropomorphic Test Device (ATD) Sustainment Parts and Factory Calibration Services
Solicitation # FA910129RB003
The United States Air Force is conducting market research to identify qualified sources capable of providing brand-new, OEM-certified replacement parts and specialized factory calibration and diagnostic services for next-generation Anthropomorphic Test Devices, specifically the Case-1 Lightest Occupant in Service and Case-6 Large Anthropomorphic Research Dummy configurations. The scope of work includes the delivery of precision structural and skeletal hardware, internal data acquisition harnesses, and the calibration of proprietary instrumentation such as Slice 6 systems, angular rate sensors, and multi-axis load cells. A critical requirement is the ability to provide a fast turnaround for services, with a target of thirty calendar days from receipt. While the government currently considers this a potential sole-source acquisition from Humanetics Innovative Solutions, Inc., this request for information seeks to determine if other businesses possess the necessary proprietary design rights, technical data, and ISO/IEC 17025 or NIST traceable certifications to fulfill these needs. Interested parties must submit a capability statement detailing their business information, technical expertise regarding component interchangeability, and their ability to integrate with Governmentwide Purchase Card ordering mechanisms. This notice is for planning purposes only and does not constitute a formal solicitation or request for proposal.
FA9101 Aedc Pkp Procrmnt Branch

POSTED

3 days ago

DEADLINE

in 4 days
View Details
NAICS: 334519
New
Federal
Waygate Video Probe System
Solicitation # 80NSSC26943709Q
NASA Shared Services Center is seeking to acquire a Waygate Video Probe System for the NASA Glenn Research Center in Cleveland, Ohio. The procurement, identified by solicitation number 80NSSC26943709Q and NAICS code 334519, is intended to be a sole source contract awarded to Waygate Technologies USA LP under the authority of FAR 12.102(a). The government is utilizing FAR Part 12 procedures for the acquisition of commercial items. The required equipment is the Everest Mentor Flex+ non-radio VideoProbe system, which includes a 5.8 inch touchscreen handset, a 6.1mm x 3.0m QuickChange VideoProbe, various interchangeable optical tips, and specialized software including InspectionWorks Connect and the MDI 2.0 workflow suite. Additional accessories such as rigidizers, a probe holder, a handset hanging hook, a hands-free mount kit, a telescoping mounting pole, and a lens cleaning kit are also required. The system must comply with specific safety and technical standards, including NPD 8710.5 and NASA Standard 8719.17 for pressure vessel and systems, as well as Glenn Safety Manual Chapter 7, paragraph 6.3 for flexible hose purchases. The expected lead time for delivery is between 1 and 10 weeks after receipt of order. While the government intends to proceed with a sole source award, it is currently requesting capability statements from interested organizations to determine if the procurement should be conducted on a competitive basis. These statements must be submitted to Procurement Specialist Laura Quave by 4:00 p.m. CST on October 14, 2026. Formal quotes will not be evaluated at this stage.
NASA Shared Services Center

POSTED

4 days ago

DEADLINE

in 1 day
View Details
NAICS: 334519
New
Federal
Vertical Launching System (VLS) Launch Sequencer (LSEQ) Multiple Award Contract (MAC) Indefinite Delivery Indefinite Quantity (IDIQ)
Solicitation # N6339426R0005
The Naval Surface Warfare Center, Port Hueneme Division is soliciting proposals for a Multiple Award Contract (MAC) under an Indefinite Delivery Indefinite Quantity (IDIQ) vehicle to procure the LSEQ MK 6 Mod 1 (NAVSEA p/n 8652144-19) and associated Lowest Replaceable Units (LRU) for the MK 41 Vertical Launching System (VLS). The scope of work encompasses the fabrication, assembly, test, and delivery of critical components, including ethernet switch modules, power tray modules, relay module assemblies, and single-mode fiber optic cable assemblies. The contract has a minimum value of 1,000 dollars per awardee and a maximum combined value of 458,090,782 dollars. The government intends to award no more than two contracts based on a best-value tradeoff process, with technical capability and capacity weighted significantly more than price and past performance. The procurement utilizes a Firm Fixed Price (FFP) structure with stepladder pricing across a five-year ordering period. Deliveries are generally scheduled for 54 weeks from the date of award and are designated as Contractor Destination. Contractors must adhere to strict quality standards, including ASQ/ANSI/ISO 9001:2015 and specific AQL levels, with final acceptance occurring within 90 days of receipt by the receiving activity. Key compliance requirements include CMMC Level requirements per DFARS 252.204-7021, strict adherence to MIL-STD-129R for marking and labeling, and the integration of Operations Security (OPSEC) into training programs. Proposals must be submitted in two separate volumes via the PIEE Solicitation Module, with a response deadline of November 24, 2026.
Commanding Officer

POSTED

4 days ago

DEADLINE

in about 1 month
View Details

More opportunities from National Aeronautics and Space Administration → NASA SBIR/STTR Program

Same awarding agency

Ready to Pursue This Opportunity?

Get AI-powered intelligence on this solicitation and the ones like it

Every page of the solicitation package shredded into a compliance breakdown

AI-powered matching based on your capabilities and past performance

Competitor and incumbent history on the requirement

Automated alerts on amendments, Q&A deadlines, and award

Miguel
Hillary
Keith Deutsch
Christine

Join 750+ contractors already using CLEATUS