| Substance | Full Form / Chemical Name | Type | Used For | Special Feature |
|---|
| CL-20 | Hexanitrohexaazaisowurtzitane | High explosive | Military warheads, missile payloads | Extremely high detonation velocity and power |
| HMX | Octogen (Cyclotetramethylene-tetranitramine) | High explosive | Shaped charges, mines, nuclear weapons | Thermally stable and more powerful than RDX |
| LLM-105 | Proprietary energetic molecule (LLNL) | Insensitive high explosive | Safer warhead compositions | Low sensitivity, high power |
| Name | Full Form / Chemical Name | Type | Primary Use | Key Features | Developed By |
|---|
| CL-20 | Hexanitrohexaazaisowurtzitane | High-performance explosive | Warheads, missiles, shaped charges | Extremely high detonation velocity, superior to HMX and RDX | U.S. Navy & China Academy of Engineering Physics |
| HMX | Cyclotetramethylene-tetranitramine (Octogen) | High explosive | Nuclear weapons, mines, IEDs, boosters | High thermal stability, more powerful than RDX | Widely used by global defense forces |
| LLM-105 | Proprietary nitro compound by LLNL | Insensitive high explosive | Safer warhead formulations | Low sensitivity, high power, safer to handle | Lawrence Livermore National Laboratory (USA) |
| Refrigerant Type | Chemical Class | Examples | GWP (Global Warming Potential) | Typical Applications | Remarks |
|---|
| Hydrofluoroolefins (HFOs) | Unsaturated HFCs | HFO-1234yf, HFO-1234ze | Very Low (~1–6) | Car AC, commercial refrigeration | Emerging low-GWP replacements |
| Ammonia (NH₃) | Natural refrigerant | R-717 | 0 | Cold storage, industrial refrigeration | Toxic and corrosive, but highly efficient |
| Carbon Dioxide (CO₂) | Natural refrigerant | R-744 | 1 | Supermarkets, heat pumps | High pressure system needed |
| Hydrocarbons | Flammable organics | Propane (R-290), Isobutane (R-600a) | Very Low (~3–20) | Domestic fridges, small AC units | Highly flammable |
| Water (H₂O) | Natural refrigerant | R-718 | 0 | Absorption chillers, experimental systems | Non-toxic, but limited to niche applications |
| Fuel Type | Chemical Composition | Used In | Remarks |
|---|
| Kerosene-based Jet Fuels | Jet Propellant-8 (JP-8), TS-1 | BrahMos, Tomahawk, Nirbhay | Standard for air-breathing engines (turbojet/ramjet) |
| Synthetic Hydrocarbons | Processed hydrocarbon fuels | Some cruise missiles | Tailored for long shelf life and high performance |
| Storable Liquid Fuels | Hydrazine derivatives (rare) | Older designs, e.g., Soviet era | Toxic, phased out in modern cruise systems |
| High Energy Density Fuels | Boron-based fuels (experimental) | Hypothetical/experimental missiles | Very high energy content, complex handling |
| Fuel Type | Propellant | Used In | Remarks |
|---|
| Solid Propellant | Ammonium perchlorate + aluminum + binder | Agni, SLBM, ICBMs | Easy to store, reliable ignition, limited control |
| Liquid Propellant (Hypergolic) | UDMH + N₂O₄ | PSLV (India, 2nd stage), old Soviet rockets | Ignites on contact, toxic, needs careful handling |
| Cryogenic Liquid Propellant | Liquid hydrogen (LH₂) + Liquid oxygen (LOX) | GSLV Mk III upper stage, Ariane 5 | High efficiency, difficult storage due to extreme temperatures |
| Hybrid Propellant | Solid fuel + liquid/gas oxidizer | Experimental systems | Combines benefits of solids and liquids; complex design |
| Green Propellants | Hydroxylammonium nitrate-based | Future space missions (NASA/ISRO interest) | Less toxic, environmentally safer replacements |