Skip to content
Skip to content

Spacecraft Fire Safety Demonstration

Metadata Updated: November 12, 2020

The objective of the Spacecraft Fire Safety Demonstration project is to develop and conduct large-scale fire safety experiments on an International Space Station resupply vehicle after it leaves the ISS and before it re-enters the Earth's atmosphere. Three Spacecraft Fire Experiment (Saffire) flight units were developed and have flown on three sequential flights of Orbital ATK's Cygnus re-supply vehicle. Saffire-I was launched on OA-6 in March 2016, Saffire-II on OA-5 in October 2016, and Saffire-III on OA-7 in March 2017.  The Saffire-I, II, and III experiments were all operated successfully in June 2016, November 2016, and June 2017, respectively. Three more Saffire experiments, Saffire-IV-VI, are now being developed to continue to investigate material flammability risks that will be faced by the crew on NASA's long duration exploration missions, especially at reduced pressure and higher oxygen concentrations. These experiments will also obtain data on large-scale spacecraft fire detection, monitoring, and post-fire cleanup as well as obtain valuable data to allow spacecraft designers and engineers to predict the development of fire scenarios in exploration vehicles and habitats. The SFS Demo Project is managed by NASA John H. Glenn Research Center (GRC) who also developed the design and fabricated the hardware. Personnel from NASA Johnson Spaceflight Center and the NASA White Sands Test Facility were also instrumental in fabricating and testing the Saffire hardware. The NASA team is augmented by an international topical team assembled by the European Space Agency (ESA). Each member of this team brings expertise and funding from their respective space and research agencies for their activities. The experiment hardware for Saffire-I-VI is approximately 53 cm x 90 cm x 133 cm and consists of a flow duct, containing the sample material to be burned, fans, and flow straightener, and an avionics bay, containing the power management system, control computer, signal conditioning card, and cameras. Saffire-I and III had a single large sample (0.4 m x 0.9 m) made of a composite fabric (75% cotton/25% fiberglass by mass) that has been studied in previous low-gravity experiments although using much smaller samples. This sample burned completely during the tests and yielded information about the fate (flame size and spread rate) of a large-scale fire in low-gravity. Saffire-II had nine samples (5-cm wide x 30-cm long) of various materials that were selected to investigate the low-gravity Maximum Oxygen Concentration (MOC) flammability limits in long-term low gravity. These samples emulate the configuration used in NASA-STD-6001 Test 1, the flammability test conducted in normal gravity to determine if a flame will spread upward over the sample or if it will self-extinguish. A material that self-extinguishes is considered as being safe for use in spacecraft from the standpoint of flammability. To conduct the Saffire experiments, the Saffire hardware is loaded in the Cygnus Pressurized Cargo Module by Orbital ATK and launched from the Wallops Flight Facility. Once at the International Space Station, Saffire remains unpowered on Cygnus while supplies for the ISS are off-loaded by the crew. Once supplies are off-loaded and replaced with trash, Cygnus departs. When the vehicle reaches a safe distance from the ISS, Saffire will be powered on by a team of Orbital ATK and Saffire engineers working from Orbital ATK's Dulles Control Center in Dulles, VA. After conducting system checks, Cygnus will be put into free drift and the experiment initiated. Saffire-I, II, and III ran autonomously for about 2-1/2 hours. With the expanded objectives of Saffire-IV-VI, the experiment will require about 8 hours to be completed. When the experiment is complete, Cygnus continues to orbit the earth while the data is downlinked to various ground stations. When downlink is complete, Cygnus will then begin its reentry into the

Access & Use Information

Public: This dataset is intended for public access and use. License: No license information was provided. If this work was prepared by an officer or employee of the United States government as part of that person's official duties it is considered a U.S. Government Work.

Downloads & Resources


Metadata Created Date November 12, 2020
Metadata Updated Date November 12, 2020

Metadata Source

Harvested from NASA Data.json

Additional Metadata

Resource Type Dataset
Metadata Created Date November 12, 2020
Metadata Updated Date November 12, 2020
Publisher Space Technology Mission Directorate
Unique Identifier Unknown
Identifier TECHPORT_13543
Data First Published 2020-12-01
Data Last Modified 2020-01-29
Public Access Level public
Bureau Code 026:00
Metadata Context
Metadata Catalog ID
Schema Version
Catalog Describedby
Harvest Object Id ea0d9e4c-3fad-4b50-8996-2d17e1d2c581
Harvest Source Id 58f92550-7a01-4f00-b1b2-8dc953bd598f
Harvest Source Title NASA Data.json
Homepage URL
Program Code 026:027
Source Datajson Identifier True
Source Hash dd758c53850807674724d4536723232b87a035ce
Source Schema Version 1.1

Didn't find what you're looking for? Suggest a dataset here.