HYDROGEN ENERGY RESEARCH
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Hydrogen Energy Research
Published 2025-01-15

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Hydrogen Energy Research
Scientific & Applied Engineering References

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Acronyms

Acronym Definition
AEM Anion Exchange Membrane: An AEM is a semipermeable membrane that allows anions to pass through while rejecting cations and gases like H2 or O2.
AEMFC Anion Exchange Membrane Fuel Cell: An AEMFC is a type of fuel cell that uses an anion exchange membrane to separate the anode and cathode compartments.
HE Hydrogen Embrittlement: Hydrogen embrittlement is the loss of ductility that many metals exhibit due to the presence of hydrogen atoms within the metal lattice.
HER Hydrogen Evolution Reaction: HER is the the cathodic process in electrochemical water splitting where H2 is adsorbed at the electrode surface, particularly involving over-potentially deposited H2 on noble metals like Pt, Rh, Ru, Ir, and Pd.
HHV Higher Heating Value: HHV is the total amount of heat released when a fuel is combusted and the products are cooled back to the fuel's original temperature. HHV includes the heat released from the condensation of water vapor that forms during combustion. HHV is also known as gross calorific value (GCV), gross energy, or upper heating value.
LHV Lower Heating Value: LHV also known as the net calorific value (NCV), is defined as the amount of heat released by fully combusting a specified quantity less the heat of vaporization of the water in the combustion product.
LH2 Liquid Hydrogen: LH2 is produced by cooling gaseous H2 to a temperature below its boiling point of -252.87°C (-423.17°F). In its liquid state, H2 is much denser than its gaseous form, which makes it easier to store and transport.
LOHC Liquid Organic Hydrogen Carrier: LOHC is an organic compound that can absorb and release H2 through chemical reactions. LOHCs store hydrogen in a liquid form by chemically binding it to the carrier molecule through a process called hydrogenation.
MCFC Molten Carbonate Fuel Cell: MCFC is a type of high-temperature fuel cell that operates at temperatures around 600°C to 700°C and uses a mixture of molten carbonate salts as the electrolyte, suspended in a porous ceramic matrix.
MEA Membrane Electrode Assembly: MEA is an essential sandwich symmetrical-structure in PEMFC, consisting of several layers of materials including a central layer of polymer electrolyte membrane inserted between two catalyst layers and then covered by two porous gas diffusion layers.
MH Metal Hydride: MH are compounds formed between metals and hydrogen and used for H2 storage because they can absorb and release H2 gas through a reversible chemical reaction.
ORR Oxygen Reduction Reaction: ORR refers to the reduction half reaction whereby O2 is reduced to H20 or H2O2. In fuel cells, the reduction to H2O is preferred because the current is higher.
PEM Proton Exchange Membrane: A PEM is a semipermeable membrane that conducts protons while blocking electrons. PEMs are used in fuel cells, where they allow protons to pass between the anode and cathode, while keeping electrons out.
SOFC Solid Oxide Fuel Cell: SOFC is a type of high-temperature fuel cell that uses a solid ceramic electrolyte to conduct oxygen ions from the cathode to the anode. Oxygen from the air is reduced at the cathode to form Oxygen ions, which then migrate through the solid ceramic electrolyte to the anode.
T&E Test & Evaluation: T&E is a crucial process to assess the performance, reliability, and safety of various systems, products, or technologies. It involves systematically examining and validating these items to ensure they meet specified requirements and perform as intended.
UAS Uncrewed Aerial System: UAS also known as a drone, is an aircraft without a human pilot onboard. It is controlled remotely or autonomously and can be used for various applications such as surveillance, delivery, agriculture, and more. When a UAS is powered by a hydrogen fuel cell, it uses hydrogen as its primary energy source.


ATOMIC / MOLAR MASS
Atomic Mass (mole): Hydrogen 1.00784 u; Carbon 12.011 u; Oxygen 15.999 u
Molar Mass: Dihydrogen 2.01568 g/mole; Carbon 12.011 g/mole; Oxygen 31.998 g/mole

HYDROGEN HEURISTICS
1000g H2(g) + 7937g O2(g) ↔ 8937g H2O(l) + 33.33kWh Energy (LHV)
3kg H2(g) + 24kg O2(g) ↔ 27kg H2O(l) + 100kWh Energy (LHV)
Light duty FCEV GH2 tank: 4-6kg H2(g)
Light duty FCEV: 1kg H2(g) / 100km
Basic filling flow rate: 1-2kg H2(g) / min
Fast filling flow rate: 14-21kg H2(g) / min
Cryogenic volumetric mass density: 70kg H2(l) / m3

HYDROGEN SHOT USA: 1kg H2 / 1USD by 2031

STOICHIOMETRY - DIHYDROGEN / ALKANES
Hydrogen Evolution Reaction (HER): 2H2O(l) ↔ 2H2(g) + O2(g) E0 = -1.229V
Gravimetric Energy Density HHV
H2 Phase Diagram
EU Copernicus
Acknowledgment of Country

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Harvard Reference Citation:
otso.com.au. (2025). Hydrogen Energy Research. [online] Available at: https://otso.com.au/ [Accessed 2025-01-15].