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Energy Storage

Lithium-ion battery concept.
Lithium-ion battery concept.
Space exploration requires electrical power and an efficient means of storing energy. This energy must be stored safely, under a wide range of environmental conditions, and for extended periods of time.

Stored energy is especially important during night time when solar energy is not available or during eclipse or periods of shadow when solar energy is blocked from reaching the solar arrays.

Energy is necessary to power rovers, tugs, habitats, experiments, beacons, astronaut tools, and in-situ resource utilization equipment, which is used to obtain material resources from lunar regolith (soil). Energy is needed to run equipment inside the space suits including liquid cooling and ventilation systems, communications equipment, bio-instrumentation and other life support systems.

NASA’s Glenn Research Center is leading the Energy Storage Project to develop energy storage technology that will enable future exploration missions to the moon and Mars. Goddard Space Flight Center, the Jet Propulsion Laboratory, Johnson Space Center, Kennedy Space Center, Marshall Space Flight Center, universities, and industry partners are collaborating with Glenn on this project. As an ongoing effort, the project team identifies new materials and manufacturing methods that will enhance the capability and safety of fuel cells and batteries. The Energy Storage Project team examines the requirements of NASA’s Constellation Program. Trade studies are conducted to determine where the team should focus their technology development efforts to address gaps between the Program requirements and performance characteristics of the current technology.

Lithium Ion Batteries

Cell Development

Li-Ion Battery Module
Li-Ion Battery Module for Mars Rovers Spirit and Opportunity.
Batteries used in automobiles and trucks contain a number of individual cells. Many batteries, such as those found in flashlights (D-cells) and TV remotes (AA-cells), are comprised of just one electrochemical cell. This project is developing advanced cell components (electrode materials, electrolytes and separators) for space-rated lithium ion cells with the following performance enhancements:
  • High specific energy - amount of energy per unit mass
  • High energy density - amount of energy stored per unit mass (The higher the energy density, the less mass that is required to provide a fixed amount of energy.)
  • Wide operating temperature range: -60ºC to +60ºC
Lithion 25 Amp-hour Battery Module

State-of-the-art is currently -20ºC to +30ºC

  • Improved reliability
  • Enhanced safety
  • Long cycle life - allows the cell to be charged and discharged many times
To improve battery safety, the Energy Storage Project is developing shut-down separators for use in lithium ion cells that would prevent thermal run-away, even under abusive conditions. Testing is performed under laboratory conditions to evaluate the behavior of these cells under abusive conditions including mishandling, puncture, overcharging, and short circuit faults.
25 Amp-hour Battery Module for Mars Lander (Mfg, Lithion Inc.).

Battery Development

image3
ABSL 18650 Li-Ion Battery Modules.
In addition to the advanced cell and cell component development, the project is designing a modular lithium-ion battery that is human-rated and meets the requirements for high energy density applications. The project team is conducting trade studies to address mass properties, safety, thermal control, and mechanical and data interfaces to create a cost effective battery design. They are also using analytical models and performing hardware testing to ensure that the battery is safe and reliable.

Once the battery is developed, the modular design can be used to support multiple exploration missions across multiple platforms. As a building block for future missions, the standardized batteries may significantly reduce life cycle costs.

Fuel Cells

Shuttle flight unit.
Shuttle flight unit.
Fuel cells are enabling technologies for many aspects of lunar surface operations. In applications where electrical power is needed for an extended period of time, fuel cells are a viable option. The total amount of energy available from a fuel cell is dependent on the size of the hydrogen and oxygen reactant tanks. The reactants feed into a fuel cell to produce electricity with drinkable water as a by-product.

Regenerative Fuel Cell (RFC) System
Regenerative Fuel Cell (RFC) System.
There are two types of fuel cells. Primary fuel cells convert oxygen and hydrogen into electrical energy and water, but stop producing electricity once the reactant supply is depleted. Regenerative fuel cells produce electrical energy in the same way as primary fuel cells. However, they are also capable of recovering the reactants by using electricity to split the product water molecules into hydrogen and oxygen in a process called electrolysis. For this process, electricity could be provided by solar arrays or a fission power system.

PEM Fuel Cells

Glenn is currently developing Proton Exchange Membrane (PEM) fuel cell technology in collaboration with Johnson Space Center, Kennedy Space Center, Goddard Space Flight Center and the Jet Propulsion Laboratory. This fuel cell chemistry is smaller and more efficient than previous types such as the alkaline fuel cells used on the Space Shuttle. Its compact size helps reduce the overall mass and volume of the spacecraft’s power system.


PEM fuel cell development unit.
PEM fuel cell development unit.

Commercial fuel cells use air as the oxidizer reactant, which has an oxygen content of only 21%. The PEM fuel cells that NASA is developing operate with an oxidizer reactant that is 100% oxygen. This means that the reactant tank only stores pure oxygen, so all of its contents can produce electrical energy (rather than only 21%). Without nitrogen in the tank, the tank can be smaller and more lightweight.

Removing water from fuel cells in the wide range of gravity environments in which space operations occur (3-g during launch to 0-g while in orbit) is currently achieved by flowing an excess of reactant gas through the fuel cell. While some of the gas reacts to make electricity, the velocity of the remaining (un-reacted) gas flowing through the fuel cell channels keeps the water moving toward the outlet. With air as the oxidizer, 80% of the gas flow through the channels does not react. When pure oxygen is the reactant, the channels must be smaller to maintain the velocity of the excess oxygen as it moves toward the outlet, carrying the water along with it. The reduced channel size (or cross sectional area) is cost effective because it results in a smaller fuel cell. When the mixture of water and un-reacted gas reach the outlet, it flows to a separator where the water is removed. The water is collected in a storage tank and the remaining reactant gas is returned to the inlet side of the fuel cell where it merges with additional reactant gas from the fuel tank before flowing into the fuel cell.

Separation of the water and air (as a reactant gas) on Earth is as simple as letting the water flow to a drain and discharging the spent air (with reduced oxygen content) into the atmosphere. In space, water separation is done with motor driven separators and mechanical pumps. While these devices are effective, they require an electrical system and maintenance, which increases the overall complexity and weight of the system. Glenn is working on separator technology that passively (without moving parts) removes liquid water from the excess oxygen stream prior to the gas being fed back into the fuel cell.

The materials from which fuel cells are made must be very durable since pure oxygen is more corrosive than air. The proton exchange membrane, fuel cell channels and other materials wetted by the reactant oxygen must all be corrosion resistant to achieve a fuel cell with long operational life. Catalyst formulations, a critical material in fuel cells, take part in the oxygen-hydrogen reaction to make electricity, but are not consumed during the process. The catalysts must also be resistant to corrosion by the flow of oxygen through the fuel cell.

Through lithium ion battery and fuel cell technology development efforts, Glenn is addressing critical energy storage requirements for spaceflight applications. Reducing weight and improving overall performance and reliability are critical to the successful deployment of fuel cells and batteries in NASA’s long-term exploration missions.


 

Contact at NASA Glenn Research Center
Chief,  Advanced Capabilities Project Office: Ann P. Over
Space Flight Systems Directorate / Advanced Flight Projects Office
216-433-6535

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Technical Writer: Emily Owens
NASA Official: Ann P. Over
Last Updated: April 16, 2008

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