Press Release

NASA Meets Key Objective in Developing New Propulsion Method

By SpaceRef Editor
December 20, 2006
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Tapping the power of 1,500 suns, scientists at NASA’s Marshall Space Flight Center have met a critical milestone in the development of aerocapture technology, a maneuver that primarily uses a planet’s atmosphere to capture a spacecraft and place it in the desired orbit.

The In-Space Propulsion Technology Project at NASA’s Marshall Space Flight Center in Huntsville, Ala., has successfully tested a series of 12-inch-square thermal protection panels. The tests focused on a type of spacecraft shielding material called an advanced charring ablator.

“The tests exposed ablators to solar power levels up to 150 watts per square centimeter — approximately 1,500 times the intensity of the sun on Earth on a clear day,” said Bonnie James, aerocapture technology manager at the Marshall Center. “This helped us simulate the high temperatures encountered by a space vehicle using aerocapture to complete a hypersonic flight through a planet’s atmosphere.”

The tests were part of a larger effort by NASA and technology developers from partnering institutions to place space vehicles into long-duration orbits around distant planets and other bodies throughout the solar system without heavy, on-board fuel loads. Instead, the nearly propellant-less method uses friction to slow a spacecraft entering the atmosphere of its destination planet. The thermal protection system shields the spacecraft from heat produced by the friction.

The tests were conducted at the Sandia National Laboratories in Albuquerque, N.M. Located on Kirtland Air Force base, Sandia’s National Solar Thermal Test Facility is a nine-acre test site with a 200-foot-tall solar tower, 212 computer-controlled mirrors called heliostats and a separate five-story control tower. The heliostats harness the power of the sun and direct it to a test sample mounted on top of the solar tower. With the total mirror area exceeding 84,000 square feet, the facility can subject specimens to up to 260 watts of thermal energy per square centimeter – about 2,600 times the intensity of the sun on Earth.

“Data from the tests are helping us determine the overall suitability of advanced thermal protection systems, adhesives and structure combinations for a future rigid aeroshell system,” said James. Aeroshells are protective “shells” that surround the spacecraft. The aeroshell and thermal protection systems under study have similar characteristics to those developed for past missions to Venus, Mars and Jupiter, along with missions to return spacecraft from the moon to Earth.

During the last three years, NASA and its partnering organizations have conducted more than 100 similar tests on samples ranging from 5-inch-diameter heat shield components to panels up to 24 inches square.

The tests also advance the technology readiness level of ablator families funded by the In-Space Propulsion Technology Program. With lower densities, higher performance and better insulative properties than current state-of-the-art technologies, these ablators have the potential to round out NASA’s current thermal protection system portfolio for aerocapture and planetary entry.

Aerocapture technology development is funded by NASA’s In-Space Propulsion Technology Program.

SpaceRef staff editor.