Constellations, Launch, New Space and more…
News

NASA’s Exo-Brake ‘Parachute’ to Enable Safe Return for Small Spacecraft

By Doug Messier
Parabolic Arc
December 16, 2016
Filed under , , , , , , ,
Engineers pack the Technology Education Satellite (TechEdSat-5) with the Exo-Brake payload. At almost 4 square feet in cross section (0.35 square meters), the Exo-Brake is made of Mylar and is controlled by a hybrid system of mechanic struts and flexible cord. (Credit: NASA Ames/Dominic Hart)

Engineers pack the Technology Education Satellite (TechEdSat-5) with the Exo-Brake payload. At almost 4 square feet in cross section (0.35 square meters), the Exo-Brake is made of Mylar and is controlled by a hybrid system of mechanic struts and flexible cord. (Credit: NASA Ames/Dominic Hart)

MOFFETT FIELD, Calif. (NASA PR) — NASA’s “Exo-Brake” will demonstrate a critical technology leading to the potential return of science payloads to Earth from the International Space Station through the deployment of small spacecraft in early 2017.

An Exo-Brake is a tension-based, flexible braking device resembling a cross-parachute that deploys from the rear of a satellite to increase the drag. It is a de-orbit device that replaces the more complicated rocket-based systems that would normally be employed during the de-orbit phase of re-entry.

“The Exo-Brake’s current design uses a hybrid system of mechanical struts and flexible cord with a control system that ‘warps’ the Exo-Brake – much like how the Wright brothers used warping to control the flight behavior of their first wing design,” said Marcus Murbach, principal investigator and inventor of the Exobrake device.

This warping, combined with real-time simulations of the orbital trajectory, allows engineers to guide the spacecraft to a desired entry point without the use of fuel, enabling accurate landing for future payload return missions.

Engineers at NASA’s Ames Research Center in California’s Silicon Valley, have been testing the Exo-Brake technology as a simple design that promises to help bring small payloads back through Earth’s atmosphere unharmed. The technology demonstration mission is a part of the Technology Education (TechEdSat-5) nanosatellite that was launched Dec. 9 on Japan’s H-II Transfer Vehicle from Tanegashima Space Center in Japan. The Exo-Brake will reside on the space station until its deployment in early 2017.

Since 2012, the Exo-Brake has been tested on balloons and sub-orbital rockets through the Sub-Orbital Aerodynamic Re-entry Experiments, or SOAREX, flight series. Earlier versions of the Exo-Brake and other critical systems also have been tested on orbital experiments on TechEdSat nano-satellite missions.

Two additional technologies will be demonstrated on TechEdSat-5. These include the ‘Cricket’ Wireless Sensor Module (WSM), which provides a unique wireless network for multiple wireless sensors, providing real time data for TechEdSat-5.

TechEdSat-5’s nanosatellite bus element will also utilize the PhoneSat-5 avionics board that uses, for the first time, the versatile Intel Edison microprocessor. The new board is designed to test TechEdSat-5’s unique Wi-Fi capabilities, high fidelity cameras, and contains Iridium L-band transceiver for data.

In addition to the goal of returning samples from the space station, the project seeks to develop “building blocks” for larger scale systems that might enable future small or nanosatellite missions to reach the surface of Mars and other planetary bodies in the solar system.

The Exo-Brake is funded by the Entry Systems Modeling project within the Space Technology Mission Directorate’s Game Changing Development program. Additional funding for the Exo-Brake is provided by NASA Ames Research Center and the NASA Engineering and Safety Center. The TechEdSat series of nanosatellites is a STEM collaborative activity that involves NASA early-career employees, interns and students from several universities including San Jose State University, University of Idaho, University of California at Riverside, and California Polytechnic San Luis Obispo.

For more information on the Game Changing Development program, visit:

https://www.nasa.gov/directorates/spacetech/game_changing_development/index.html

For more information on NASA’s small satellite missions, visit:

https://www.nasa.gov/smallsats

Kimberly Williams
Ames Research Center

8 responses to “NASA’s Exo-Brake ‘Parachute’ to Enable Safe Return for Small Spacecraft”

  1. Kapitalist says:
    0
    0

    If it for example is used to take a sample of Venus’ atmosphere and then again to soft land on Earth, it doesn’t matter where it takes the sample at Venus and one can certainly find it where ever it lands on Earth. Would have to be a bit bigger than illustrated here and have a heating and crashing safe sample container. But it would still be a minisat.

    I think this stuff, in combination with Solar sails and secondary payload launch providers offering chemical propulsion services (which traditionally has not been allowed on secondary payloads because of the risk to other cargo) could be really great especially for Venus but also for Mars exploration.

    • publiusr says:
      0
      0

      I think this is just about helping end of life spacecraft re-enter and burn up sooner so as to reduce space junk. No heat shield that I can see at least.

      • Christopher James Huff says:
        0
        0

        It’s explicitly stated that it’s about guiding payloads being returned to Earth from the ISS to a precise reentry without the use of rocket propulsion. You don’t see a heat shield because they’re not developing a heat shield. They don’t need to develop a shielded payload to test their deorbit system…we already know how to solve that part of the problem.

  2. DougSpace says:
    0
    0

    I’m seeing what looks like struts that could steer the chute so perhaps some guidance. It could have a low ballistic coefficient so, with its chute deployed, perhaps it could decelerate sufficiently to survive re-entry. After all, safe return of payload is what they are claiming. With low mass, a parachute, and steerability, perhaps they could be aimed at a desert location and use their parachute to glide to a specific location. No need for air or sea recovery.

  3. DougSpace says:
    0
    0

    I take that back. It has four flaps not two so I now don’t see any maneuverability.

  4. therealdmt says:
    0
    0

    I’ll be looking forward to seeing this demonstrated. This could help increase the utility of LEO research and, as others are pointing out, could be applicable to other destinations with atmospheres (Mars, Venus, Titan). There could also be other applications, such as deorbiting space junk or (slow mo) orbital changes, all at the cost of no propellent.

Leave a Reply