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Advanced Propulsion

Advanced Propulsion. Slingshot Orbits:. The stationary or resonant orbits give spacecraft consistent positioning while expending the minimum energy. However we can also use orbits to accelerate to greater velocities.

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Advanced Propulsion

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  1. Advanced Propulsion

  2. Slingshot Orbits: The stationary or resonant orbits give spacecraft consistent positioning while expending the minimum energy. However we can also use orbits to accelerateto greater velocities. • The best example of a slingshot’s usefullness comes from the Cassini spacecraft. • Cassini flew a ‘VEGA’ orbit where it stole momentum from Venus, Venus again, Earth, and finally Jupiter on its way to Saturn. • The ‘GA’ in VEGA comes from an asteroid (Gaspra) that Cassini came close to….no slingshot though.

  3. Fuel Velocity: The second paradigm for improving our flight performance is to increase the speed of our exhaust. • The rocket shows that our ultimate velocity increases linearly with the velocity of our fuel. It’s the most efficient way to improve things. • We mainly rely on a single method of achieving thrust, but there are several advances on the horizon that are in various stages of development.

  4. Types of Fuel: There are three main types of physical process that we use for fuel in space propulsion. • Chemical Reactions: This amounts to triggering an energy releasing chemical reaction in a controlled (or uncontrolled) way. (By far the most common method). • Plasma Reactions: These thrusters use electric fields to accelerate ions. (Not used for launches, but more common now in trajectory corrections). • Nuclear Reactions: Nuclear propulsion relies on fission power to generate massive amounts of energy that propel exhaust at huge speeds. (Hard to control, but can also be an impulse drive).

  5. Chemical Fuel: Chemical fuels are the most common, but also the least efficient. • Water: Many liquid fuel rockets use the formation of water to generate thrust. H2 + O  H2O + energy! • Water reactions produce exhaust speeds of 3-4 km/sec. • So, what does it take to get the Apollo capsule to the Earth escape velocity of 11 km/sec?

  6. Fuel Velocity: Chemical fuels are the most common, but also the least efficient. • The Apollo payload weighed 47000 kg. • We can solve the Rocket equation for mfuel to get that we need the equivalent of 726000 liters of water!!!! • Even the most advanced chemical propellants produce exhaust no faster than 5 km/sec. Plus, these reactions are pretty dangerous!

  7. Fuel Velocity: Chemical fuels are the most common, but also the least efficient. • What if we could get the fuel speed up to 11 km/sec? • We can solve the Rocket equation for mfuel to get that only need 80000 liters of water. That’s a factor of nearly 10x!!!! • So speed is important!

  8. Thrust Alternatives: There are many ways to improve over chemical rockets for fuel velocity, some of which are even in use today. • The most common of these technologies is a broad class of device called a plasma thruster. • Plasma thrusters operate by accelerating ions away from a payload at high velocity. • They generally carry only a little fuel with them, but make up for it with Vex.

  9. Electrostatic Ion Thrusters: EIT designs use an electron gun (similar to a CRT) to fire ions through a grid and into space. • EIT devices have been used for many years in spacecraft. Their most visible role was in the NASA Deep Space 1 mission. • Velocities from ion thrusters can be very large (250 km/sec has been achieved). • Such a device could lift an Apollo style payload to escape with only 2100 kg of fuel! (0.3% of a Saturn V).

  10. Electrostatic Ion Thrusters: EIT designs use an electron gun (similar to a CRT) to fire ions through a grid and into space. • EIT devices have been used for many years in spacecraft. Their most visible role was in the NASA Deep Space 1 mission. • Unfortunately they will burn out their electron gun long before they can produce that much V.

  11. Electrostatic Ion Thrusters: EIT designs use an electron gun (similar to a CRT) to fire ions through a grid and into space. • EIT devices have been used for many years in spacecraft. Their most visible role was in the NASA Deep Space 1 mission. • They are also pretty slow in accelerating things. Typical forces are about equal to the weight of a sheet of paper in your hand.

  12. Helicon Thrusters: A group at the University of Washington is developing a different kind of plasma thruster called a ‘Helicon Thruster’ . • Helicons work by using magnetic ‘waves’ to create and accelerate plasma. There’s no electron gun to break down. • HTs can overcome some of the limitations of EIT devices and are in active development worldwide.

  13. VASIMR: The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is an advanced helicon design being developed by NASA. • VASIMR is a hydrogen helicon engine being built by AdAstra Rocket corp. for NASA. • VASIMR is a controlled helicon that can be used for different amounts of thrust at different times in a mission. • It still suffers from low forces, but they add up over a flight.

  14. VASIMR: The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is an advanced helicon design being developed by NASA. • VASIMR is a hydrogen helicon engine being built by AdAstra Rocket corp. for NASA. • VASIMR uses hydrogen because it could be refueled once it reached a target like Mars. • Reducing the amount fuel is a goal, but there are compromises with this design. Why would Hydrogen be a poor choice?

  15. Nuclear Propulsion: Nuclear engines are another broad class of devices that use fission (or fusion!) energy to produce thrust. • We already know that nuclear power has far more energy/mass than chemical reactions. • If there’s more energy per mass, then the kinetic energy (1/2MV2) of the exhaust will be greater. • In theory you can increase your exhaust velocity using nuclear energy by square root of the energy capacity. Up to thousands of times more in the case of fusion.

  16. Nuclear Generators: We use nuclear power already for both ground and space transportation. • The most prominent use is the Radioisotope Thermal Generator (RTG). • RTGs have a good service history, but are still controversial.

  17. NERVA: An early design for a nuclear rocket was the Nuclear Engine for Rocket Vehicle Application. • NERVA was intended as a replacement for the Saturn V third stage. • NERVA was FAR more controversial than a RTG and was cancelled in 1972.

  18. Prometheus: Project Prometheus is a recent attempt to mate nuclear power to plasma trust technology in a system that would use fission to power and move a spacecraft. • Prometheus would have been used initially on an ambitious mission to Jupiter (the Jovian Icy Moons Orbiter-JIMO). • A Prometheus spacecraft would have 100s of times more energy to use than current designs. • It would be able to move between targets with its greater thrust-fuel ratio.

  19. Prometheus: Project Prometheus is a recent attempt to mate nuclear power to plasma trust technology in a system that would use fission to power and move a spacecraft. • Prometheus would have been used initially on an ambitious mission to Jupiter (the Jovian Icy Moons Orbiter-JIMO). • Prometheus was part of the Bush Administration 2002 plan for the future of space. • Prometheus wasn’t part of the Bush Administration 2004 plan for the future of space. • More than 80% of its funding has been cut…future unclear.

  20. Orion: Orion is an advanced concept for nuclear spaceflight dating back to the 1940s. • Orion spaceships operate by detonating nuclear bombs behind the payload. • This generates a HUGE amount of thrust that could accelerate massive payloads to 10-20% of the speed of light. • Orions could explore the solar system easily and even visit nearby star systems. • Nukes in space are REALLY controversial though.

  21. No Fuel Designs: As nice as nuclear and ion propulsion are, the most efficient way to travel would be to carry no fuel at all. • NASA has supported several designs to travel in space without carrying any (or minimal) fuel. • One technique is called Solar Thermal Propulsion. STP still carries fuel, but uses mirrors to heat it and generate thrust. It’s much more efficient than chemical rockets.

  22. The Solar Sail: Solar Sails have been discussed as a means of space travel for a long time. • Solar sails work like wind sails, but with radiation pressure (momentum from light) as the ‘wind’. • Solar Sails are conceptually simple • Several test flights have already occurred with them, but all have failed for reasons unrelated to the feasibility of the technique. • Criticisms of the technique include steering and the reduction in ‘fuel’ with distance from the Sun.

  23. Magnetospheric Propulsion: A University of Washington effort has been involved in developing a new class of ‘solar sail’ that uses the solar wind. • Called M2P2, this device works by creating a magnetosphere around a spacecraft that then interacts with the solar wind. • The solar wind has much less momentum than solar radiation, but the fields can be made very large.

  24. Magnetospheric Propulsion: A University of Washington effort has been involved in developing a new class of ‘solar sail’ that uses the solar wind. • Called M2P2, this device works by creating a magnetosphere around a spacecraft that then interacts with the solar wind. • M2P2 has been demonstrated in the lab to work.

  25. Magnetospheric Propulsion: A University of Washington effort has been involved in developing a new class of ‘solar sail’ that uses the solar wind. • M2P2 has also been suggested as a way to send un-fueled spacecraft to various places in the solar system. • An added benefit is that the magnetic field will shield the crew!

  26. The Bussard Ramjet: The ramjet is a spacecraft that picks up its fuel along the way. • The Bussard design would scoop up ions and accelerate them out the back. • The greater the difference between the local plasma velocity and the spacecraft, the more thrust is obtained.

  27. The Scramjet: NASA is actually building a version of a ramjet that works in the atmosphere. • The X-43 works by taking in Oxygen in the air and mixing it with onboard Hydrogen to produce thrust. • Very high speeds are required to start this process, more than 3000 mph!

  28. Space Elevator: Nearly all of the methods described here do not work for an Earth launch event. • A space elevator is an idea that’s simple in concept but seems impossible to achieve. • All you need to do is run a cable from the ground to a counter weight near a GSO point. • Payloads then ‘climb’ up the cable and into orbit!

  29. Space Elevator: A local company is working to build a space elevator. • Their concept would put the base of the elevator on a series of boats in the ocean. • The primary technical challenge is to find a material strong enough to make the cable.

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