History
LOFTID is the latest in a string of successful Hypersonic Inflatable Aerodynamic Decelerator ( HIAD) development efforts. HIADs have a Viking-era genesis; developed by engineers at the NASA Langley Research Center as a possible system for crewed reentry. However, HIAD development ceased in the mid-1970s when it was shown disk-gap-band supersonic parachutes were suitable for the Viking, Pioneer Venus and Galileo mission environments. More recently, the need to enable robotic and crewed missions with larger payload mass has generated new investment in HIAD development. Starting in 2006 with the Program to Advance Inflatable Decelerators for Atmospheric Entry (PAIDAE), HIADs have undergone a series of incremental development efforts including design and analysis, ground based materials testing, manufacturing, wind-tunnel testing and flight tests and demonstrations. Two successfulDesign
It inflates to 6 metres (about 20 feet) in diameter. Its total mass is about 2,400 lb. It is formed from 7 inflatable tori (6 wide and one narrow), with a flexible woven silicon carbide black ceramic fabricLOFTID cutawayLaunch, deployment, and results
Launch and deployment (inflation, separation and splashdown from the Atlas V Centaur 2nd stage) were successful. It reentered the atmosphere at about Mach 29, reached a peak deceleration of about 9 g, and splashed down under a subsonic parachute near Hawaii. NASA stated on November 17 that LOFTID was a "huge success" and able to be used on future missions to Mars. According to the principal investigator, Dr. Neil Cheatwood, the success means the technology is now ready to use on missions.Commercial interest
Dr. Cheatwood reports that about a dozen companies have contacted him to express interest in the technology.See also
* Inflatable decelerator, including NASA's IRVE and HIADReferences
{{NASA-stub NASA programs Spaceflight technology Inflatable aircraft