Which fuel is used in rockets?

Let’s go in detail about the fuels used in rockets:

Which fuel is used in rockets?

1. Definition of Rocket Fuel

Rocket fuel is a substance that reacts chemically (or decomposes) to produce thrust for propelling a rocket.

  • Unlike car or airplane fuel, rocket fuel must provide extremely high energy and work in space or near-vacuum conditions.
  • Rocket fuel is classified as liquid, solid, or hybrid, depending on its physical state and application.

2. Types of Rocket Fuel

A. Liquid Rocket Fuel

  1. Liquid Bipropellant Fuel
    • Consists of a fuel and an oxidizer stored separately.
    • They react when combined in the combustion chamber to produce high thrust.

Common Examples:

FuelOxidizerNotes
Liquid Hydrogen (LH2)Liquid Oxygen (LOX)Used in NASA’s Space Shuttle main engines
Kerosene (RP-1)Liquid Oxygen (LOX)Used in Saturn V first stage and SpaceX Falcon 9
Hypergolic fuels (e.g., Hydrazine, UDMH)Nitrogen Tetroxide (N2O4)Ignite on contact, used in satellites and orbital maneuvers
  1. Advantages:
    • High specific impulse (efficiency)
    • Throttleable and restartable engines
  2. Disadvantages:
    • Complex storage and cryogenic handling
    • Toxicity and cost

B. Solid Rocket Fuel

  • Pre-mixed fuel and oxidizer in solid form.
  • Commonly used in boosters and missiles.

Examples:

  • Ammonium Perchlorate / Aluminum (used in Space Shuttle Solid Rocket Boosters)
  • Composite propellants with polymer binders

Advantages:

  • Simple, stable, easy to store
  • High thrust at ignition

Disadvantages:

  • Cannot be throttled or shut down easily
  • Less efficient than liquid fuel

C. Hybrid Rocket Fuel

  • Combines solid fuel with a liquid or gaseous oxidizer.
  • Example: Hydroxyl-terminated polybutadiene (HTPB) with liquid oxygen or nitrous oxide

Advantages:

  • Safer than fully liquid propellants
  • Can be throttled to some extent

Disadvantages:

  • Less mature technology compared to solid/liquid fuels

3. Characteristics of Rocket Fuel

PropertyImportance
High Energy DensityProduces large thrust from small volume
Ignition ReliabilityMust ignite under extreme conditions
StabilityCan be stored safely until launch
Compatibility with Engine MaterialsPrevents corrosion or damage
Specific Impulse (Efficiency)Determines how much thrust per unit mass of fuel

4. Summary

  • Rocket fuel types:
    1. Liquid fuels – e.g., LH2/LOX, RP-1/LOX, hypergolic fuels
    2. Solid fuels – e.g., ammonium perchlorate-based composites
    3. Hybrid fuels – combination of solid fuel and liquid/gas oxidizer
  • Liquid fuels: High efficiency, throttleable, complex handling
  • Solid fuels: Simple, reliable, high thrust, not throttleable
  • Hybrid fuels: Safer and partially controllable
  • Rocket fuel is completely different from automotive or aviation fuel because it must operate in space and generate extreme thrust.

💡 Tip:

  • Automobiles use chemical fuels for air-breathing engines, while rockets carry both fuel and oxidizer because there is no atmospheric oxygen in space.

Other courses:

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