Inflatable heat shield could deliver heavy payloads to worlds with a thick atmosphere

One of the greater challenges of sending payloads to Mars is contending with the planet's atmosphere. While incredibly thin compared to Earth's (with roughly half of 1 percent of Earth's air pressure), the resulting air friction is still an issue for spacecraft looking to land there. And looking to the future, NASA hopes to land heavier payloads on Mars, as well as other planets—some of which may have atmospheres as dense as Earth.

A possible solution to this is the use of inflatable aeroshell heat shields that offer advantages over rigid ones. To develop this technology, NASA and United Launch Alliance (ULA) have partnered to develop an inflatable heat shield known as the Low-Earth Orbit Flight Test of an Inflatable Decelerator (LOFTID). By 2022, they hope to send this cutting-edge prototype to low-Earth orbit (LEO), where it will be tested.

When a enters an atmosphere, aerodynamic forces exert drag upon it. This slows the spacecraft down, converting its kinetic energy into heat. Naturally, this heat can become very intense, posing a threat to the spacecraft and any crew it may have aboard. Thus, payloads and crewed missions are equipped with heat shields to protect them during atmospheric entry.

Since its inception in 1958, NASA has relied heavily on retro-rocket propulsion and rigid heat shields to decelerate spacecraft during orbital entry, descent and landing (EDL) operations. Unfortunately, these systems come with their share of drawbacks, not the least of which is mass and the need for propellant. At the same time, scalability is a bit of an issue since larger payloads require a larger aeroshell, which means even more mass.

This is where inflatable shields are especially useful. Using this technology, NASA and other space agencies would be able to use larger aeroshells that could produce more drag while saving on mass. By incorporating ideas like LOFTID, which utilize aerodynamic forces instead of propulsion, NASA stands to revolutionize the way it delivers payloads to planets and into orbit.

Credit: NASA

The concept is an example of hypersonic inflatable aerodynamic decelerator (HIAD) technology, which NASA has been researching for over a decade. HIAD not only provides the most mass-effective way to decelerate a spacecraft entering a planet with an atmosphere, but also overcomes the packaging limitations of rigid systems by utilizing inflatable materials that can be stowed within the launch vehicle.

This technology is therefore the most mass-effective way to decelerate a spacecraft entering a planet with an atmosphere, and could deliver larger masses to any elevation on the planet. Having conducted two suborbital flight tests, the LOFTID orbital flight test (in 2022) is the next logical step in the proving process since it will allow the technology to be validated for a number of mission applications.

Once testing is completed and the technology can be integrated, LOFTID and other HIAD concepts could enable missions to other planets and bodies in the solar system, as well as locations that are higher in elevation. It could also be used for payloads and crews returning from the International Space Station (ISS) to Earth, as well as for recovering reusable components such as the engines on the ULA's proposed Vulcan rocket.

Tests are still ongoing at NASA's Langley Research Center, where engineers are preparing the for launch. This consists of measuring the temperature of nitrogen gas as it vents from the tanks that will be used during the maiden test flight. Pack and deployment testing is also being conducted by Airborne System, a parachute design and manufacturing company in Santa Ana, California.

If all goes well with the orbital test in 2022, we can expect that HIAD-type aeroshells will become a regular feature for missions to Mars, Venus, Titan, and other bodies in the solar system that have denser atmospheres.

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Citation: Inflatable heat shield could deliver heavy payloads to worlds with a thick atmosphere (2019, June 18) retrieved 15 August 2020 from
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