Ullage motor

From Wikipedia, the free encyclopedia
  (Redirected from Ullage engine)
Jump to: navigation, search

Ullage motors (also known as ullage engines or ullage rockets) are relatively small, independently fueled rocket engines that may be fired to accelerate the rocket prior to main engine ignition, when the vehicle is in a zero-g situation.


Three sets of ullage motors are shown in this schematic of the Saturn V rocket

Cryogenic-liquid-fueled rockets keep their propellants in insulated tanks. These tanks are never completely filled to allow for expansion. In micro-gravity conditions the cryogenic liquids are without a free surface existing in a slushy state between solid, liquid, and gas. In this mixed state, ullage gases may be sucked into the engines, which is undesirable. Small rocket engines, called "ullage motors", are sometimes used to settle the propellant prior to the main engine ignition to allow the formation of a temporary free surface (with a distinct boundary between liquid and gas states). These motors provide acceleration that moves the main engine liquid propellants to the bottom of their tanks ("bottom" in this usage always meaning relative to the alignment of the main motor the ullage motors are serving), so they can be pumped into the engine plumbing. The Agena-A was one of the first vehicles to make use of an ullage system in preparation for ignition after separating from its Thor booster.[1] Failure of the Agena's internal timer was also blamed for premature ignition of this ullage system in the failed launch of "Discoverer Zero" on January 21, 1959.[2] Such motors were also used by Soviet engineers for the Molniya interplanetary launch vehicle in 1960.

The firing of the ullage motors is used during stage separation of rocket and/or stabilization of a rocket when there are brief reductions in acceleration which could allow the liquid propellant to float away from the engine intakes. Ullage motors are also commonly employed on deep-space missions where a liquid rocket needs to start a burn after traveling in micro-gravity.

Ullage motors are typically very small; research[by whom?] shows that accelerations of the order 0.001 g are needed to avoid excessive gas intake. Some vehicles use other techniques to hold liquid at the inlet, as once the main engines are ignited, ullage motors are no longer required.

The second stage (S-II) of the Saturn V rocket used in the American Apollo program used four (originally eight) ullage motors located on the aft interstage skirt. In the S-IVB third stage, there was an Auxiliary Propulsion System that also had ullage functions. Ullage is often a secondary function of the reaction control system such as on the Apollo Lunar Module (LM). In his book Lost Moon, Jim Lovell recounted a description of a course-correction burn of the LEM's main descent engine to re-enter a free return trajectory to Earth during the successful recovery of the Apollo 13 capsule:

When the ship had stabilized in the proper attitude for firing, Lovell would deploy the LEM's landing gear, extending its four spidery legs to get them out of the way of the descent engine. Next the computer, relying on other instructions Haise typed into it, would fire four of Aquarius's attitude jets for 7.5 seconds. This procedure, known as ullage, was intended to jolt the spacecraft slightly forward and force the descent engine fuel to the bottom of its tanks, eliminating bubbles and air pockets. After that, the main descent engine would ignite automatically firing at 10 percent thrust for 5 seconds.[3]


  1. ^ "Discoverer I System Test Evaluation Report" (PDF). National Reconnaissance Office. Retrieved 15 March 2015. 
  2. ^ Philip Taubman, 2003; "Secret Empire", p721; ISBN 0-684-85699-9
  3. ^ Jim Lovell & Jeffrey Kluger, 1994;"Apollo 13 (previously titled: Lost Moon)", p176; ISBN 0671-53464-5