Hypersonic Inflatable Heat Shield Tested Successfully

by Nancy Atkinson on July 23, 2012

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Caption: IRVE-3 was launched by a sounding rocket at 7:01 a.m. Mon., July 23, from NASA’s Wallops Flight Facility. Credit: NASA.

A prototype for a large inflatable heat shield that could one day be used for landing large payloads on Mars was tested successfully on July 23, 2012, surviving a hypersonic speeds through Earth’s atmosphere. The Inflatable Reentry Vehicle Experiment (IRVE-3) traveled at speeds up to 12,231 km/h (7,600 mph) after launching on a sounding rocket from NASA’s Wallops Flight Facility on Wallops Island, Virginia.

“We had a really great flight today,” said James Reuther, deputy director of NASA’s Space Technology Program, after the test flight. “Initial indications are we got good data. Everything performed as well, or better, than expected.

Watch the video from the flight below.

IRVE-3 is a cone of uninflated high-tech rings covered by a thermal blanket of layers of heat resistant materials. NASA said the purpose of the IRVE-3 test was to show that a space capsule can use an inflatable outer shell to slow and protect itself as it enters an atmosphere at hypersonic speed during planetary entry and descent, or as it returns to Earth with cargo from the International Space Station. A larger version has been proposed for landing larger payloads on Mars, such as future human missions.

About 6 minutes into today’s flight, as planned, the 680-pound inflatable aeroshell, or heat shield, and its payload separated from the launch vehicle’s 55 cm (22-inch)-diameter nose cone about 450 km (280 miles) over the Atlantic Ocean.

An inflation system pumped nitrogen into the IRVE-3 aeroshell until it expanded to a mushroom shape almost 3 meters (10 feet) in diameter. Then the aeroshell plummeted at hypersonic speeds through Earth’s atmosphere. Engineers in the Wallops control room watched as four onboard cameras confirmed the inflatable shield held its shape despite the force and high heat of reentry. Onboard instruments provided temperature and pressure data. Researchers will study that information to help develop future inflatable heat shield designs.


Caption: Technicians prepare the Inflatable Reentry Vehicle Experiment (IRVE-3). Credit: NASA

A Navy crew will attempt to retrieve the aeroshell.

“It’s great to see the initial results indicate we had a successful test of the hypersonic inflatable aerodynamic decelerator,” said James Reuther, deputy director of NASA’s Space Technology Program. “This demonstration flight goes a long way toward showing the value of these technologies to serve as atmospheric entry heat shields for future space missions.”

IRVE-3 is part of the Hypersonic Inflatable Aerodynamic Decelerator (HIAD) Project within the Game Changing Development Program, part of NASA’s Space Technology Program.

Source: NASA

About 

Nancy Atkinson is Universe Today's Senior Editor. She also is the host of the NASA Lunar Science Institute podcast and works with Astronomy Cast. Nancy is also a NASA/JPL Solar System Ambassador.

zkank July 24, 2012 at 5:34 AM

Maybe this technology can be also developed into some type of inexpensive lifeboat for orbiting stations in the future.

Currently, only Russia and China are able to bring humans to and from space.
Should a desperate situation occur, it would be nice to have one of these shells available to get down in a hurry.
Better than nothing!

morphics July 24, 2012 at 12:45 PM

Just add some spacesuit boot bindings and you could surf this baby all the way to the surface!

Torbjörn Larsson July 24, 2012 at 1:28 PM

Some of the same technology was proposed to make individual “descent bubbles” that would take an astronaut through the hot part before making a final chute drop. It seems to have originated in scifi (Heinlein’s “Star Trooper” is the first one I know of), but the principle is sound.

It has a lot of uses. Sample return and manned missions would like to drop off orbiters such as communication relays and return vehicles. If it works it could perhaps even be feasible as a dual use transferable aerobrake&descent shield for the whole mission with a temporary staging orbit before descent, saving fuel and structural mass.

zkank July 24, 2012 at 9:12 PM

(I see we enjoy some of the same books)

Bang on!
Starship Troopers novel, 1959 well ahead of its time – much different than the movie, really does an excellent job describing the shelled descent by the soldiers, eh?
Multi-layers discarded for multiple advantages.

As a sci-fi fan, I always enjoy seeing the foresight coming to fruition, which seems to be quite often these days!

Aqua4U July 24, 2012 at 11:23 PM

Yes, that’s right… Trick would be to make the inflatable Mars entry balloot module part of a 1 G spun habitat for use during transit? Think ‘transformer’ style accommodations? After landing.. the same is used for inflatable garage and/or base ops.

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