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Advanced Chemical Technology Overview

Chemical propulsion systems have historically been the primary means for transportation of payloads in space because they generate the very large amounts of thrust required to overcome the effect of Earth's gravity.

Technology Benefits:
  • Increased performance and safety
    Application of high Isp storable cryogenic propellants to enable long-term missions in space
    Accommodate extended missions without propellant losses
    Advanced fuels with improved performance (increased Isp) could minimize need for aerobraking
    Advanced Chemical
    Aerojet Bi-propellant Hot-fire Test

  • Reduced propellant storage uncertainties
    Reduced launch mass, or
    Increased payload capability to enhance science missions

  • Improve overall system efficiency (Thermal/Pressure control)
    Pressure control / venting without auxiliary propulsion resettling
    Better vehicle cooling and reduced cryogenic boil-off
    Cross-benefits for other propulsion systems

  • Technology Status:
    Many advanced chemical propellants are being analyzed and tested to determine their performance and applicability to in-space propulsion. Chemical rocket systems include solid, cryogenic liquid, and storable liquid propellants, as well as hybrid and cold gas rockets. The number of compounds used in the reactions typically categorizes these propellants. Researchers are investigating ways to increase Isp, lifetime and overall performance of state-of-the-art chemical systems.

Future Plans / Challenges:

  • Advanced Fuels
    Evaluate high-energy storable propellants that will enhance performance for in space application

  • Cryogenic Fluid Management
    There are many aspects in the loading, storage, and pumping of cryogenic fluids currently being analyzed and augmented in order to improve the efficiency and safety of handling these materials. Some of the major areas of investigation are:
    • Zero-G pressure control/Capillary Liquid Acquisition Devices
    • On-orbit Propellant transfers, including filling the vehicle upper stage during ascent
    • Liquid Mass Measurement
    • Cryogenic Storage with both passive and active heat removal
    • Zero Boil-Off Tank Pressure Control

    Typically, these efforts concentrate on conducting analysis, building simulations, constructing test fixtures, building scaled and full-size equipment, and finally verification of the analysis and simulations through testing. The safe and efficient utilization of cryogenic fluids for engines, thrusters, and life support systems continues to be a major investment area for the IISTP.

  • Lightweight Components
    Reducing the weight and complexity of the structures used to carry chemical propellants is also vital in increasing payload capabilities. Liquid propellants all require holding vessels along with complex piping and mixing apparatus. The combination and combustion chambers tend to be large and heavy. Advanced materials are being developed that will reduce the size and weight of the components, thus directly increasing payload capability.
 
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