The Bussard ramjet method of spacecraft propulsion was proposed in 1960 by the physicist Robert W. Bussard and popularized by Carl Sagan in the television series and subsequent bookCosmos as a variant of a fusion rocket capable of fast interstellar spaceflight. It would use a large scoop (on the order of miles) to compress hydrogen from the interstellar medium and fuse it. To save mass, some people have suggested using a magnetic field for a scoop. More recent calculations have shown that the drag of a scoop would be more than the thrust generated by the fusion reaction. However, the calculations (by Robert Zubrin and an associate) inspired the idea of a magnetic parachute or sail. Sagan called the construction of such a ship "engineering on the scale of small worlds".
There may be practical modifications of this concept. For example, perhaps one could shoot nuggets of fuel in front of a spacecraft from a fixed base, and then the spacecraft would not have to accelerate its own fuel. More speculatively, if the hydrogen was somehow fed into the engine and fused without being accelerated to the spacecraft's current velocity first, there would be no drag. A problem that must be overcome is that most interstellar hydrogen is ordinary protium, instead of the easier_to_fuse deuterium and tritiumisotopes, and so makes a poor fusion fuel; it is possible that this could be overcome by using a carbon–nitrogen–oxygencatalysed nuclear cycle. Potential relative velocities of such a ship are theorized to exceed 16 per cent (0.16) of the speed of light.
The Bussardramjet method of spacecraft propulsion was proposed in 1960 by the physicist Robert W. Bussard and popularized by Carl Sagan in the television series and subsequent book Cosmos as a variant of a fusion rocket capable of fast interstellar spaceflight.
The typical velocity of the interstellar wind is 50 km/s beyond the heliopause.
In Coyote by Allen Steele the Starship Alabama uses a Bussardramjet for propulsion on the journey to 47 Ursae Majoris.
In a ramjet, owing to the high flight speed, the ram compression is sufficient to dispense with the need for a compressor and a turbine to drive it.
Ramjets generally give little or no thrust below about half the speed of sound, and they are inefficient (less than 600 seconds due to low compression ratios) until the airspeed exceeds 1000 km/h (600 mph).
Ramjets are found almost exclusively in missiles, where they are boosted to operating speeds by a rocket engine, or by being attached to another aircraft (typically a fighter).