QUOTE (Alex01 @ Dec 9 2007, 09:29 AM)

If I'm not mistaken, rockets use Solid Rocket Fuel (SRF), this solid rocket fuel allows the rocket's engine to burn even with a lack of oxigen. That's how many of todays rockets get into orbit.
The shuttle's Solid Rocket Boosters (SRB) also use this kind of fuel to produce propulsion.
Of course I could be wrong.

There are several types of boosters. The Russians and Chinese use liquid fuels, as did Saturn rockets.
This is about that "yellow flame" (?) picture. I don't really uinderstand the question. Many rocket flames can also burn blue. There are retrorockets firing in that picture, adding to the exhaust profile.
"The Saturn I second stage, called S-IV, was powered by a Pratt and Whitney engine fuelled by LOX and liquid hydrogen.
In a typical Saturn V Apollo flight, the five F-1 first stage engines were ignited 6 sec before liftoff. The center F-1 engine was shut down 135 sec after launch and the outer four F-1 engines 15 sec later. One second following cutoff of the four outer F-1 engines, the first stage separated. Simultaneously, eight retrorockets were fired briefly to slow the first stage and prevent it bumping into the second stage. Following separation, the spent first stage fell into the Atlantic about 640 km downrange.
One second after first stage separation, eight solid-fueled motors mounted on the first/second stage adapter ring were fired for 4 sec. As well as maintaining the positive motion of the rocket, this forced the second stage fuel to the bottom of its tanks in order to feed the engines – a so-called ullage maneuver – and was the cue for the five J-2 second stage engines to ignite.
Thirty seconds later, the first/second stage adapter ring fell away, and six seconds after that, the escape tower was jettisoned. The second stage engines burned for 365 sec before the next separation took place.
Four solid-fueled retrorockets on the second stage fired to keep the second and third stages from colliding. Then the second stage began its drop into the Atlantic about 4,000 km from the launch site.
At this point, the Saturn V was traveling about 25,300 km/h at an altitude of 185 km. Two solid-fueled motors on the third stage aft skirt were fired briefly to settle the fuel and simultaneously, the S-IVB third stage J-2 engine fired up for a burn of 142 sec. This initial S-IVB burn carried Apollo into a 190-km orbit at a speed of 28,200 km/h.
Thirty seconds later, the first/second stage adapter ring fell away, and six seconds after that, the escape tower was jettisoned. The second stage engines burned for 365 sec before the next separation took place.
Four solid-fueled retrorockets on the second stage fired to keep the second and third stages from colliding. Then the second stage began its drop into the Atlantic about 4,000 km from the launch site.
At this point, the Saturn V was traveling about 25,300 km/h at an altitude of 185 km. Two solid-fueled motors on the third stage aft skirt were fired briefly to settle the fuel and simultaneously, the S-IVB third stage J-2 engine fired up for a burn of 142 sec. This initial S-IVB burn carried Apollo into a 190-km orbit at a speed of 28,200 km/h."
-David Darling
Video