ISS Propulsion Module
From Wikipedia, the free encyclopedia
An ISS Propulsion module was proposed as a backup to functions performed by the Zvezda Service Module and Progress spacecraft. Critical ISS GN&C/Propulsion functionality only resides in Russian (Zvezda and Progress) and future European (ATV) assets. A Propulsion Module would have been needed for ISS altitude maintenance and reboost, debris avoidance maneuvers, attitude control and propellant supply in the event the Zvezda Service Module was not available (launch failure, etc) to the International Space Station. If the Zvezda had not been available, the Interim Control Module would have been used at first. It only had a lifetime of 3 years; then the Propulsion Module would have been necessary.
The ISS needs an average of 7000 kg of propellant each year for altitude maintenance, debris avoidance and attitude control. It will need 105,000 kg through 2014.
A Propulsion Module would have provided reserve propellant for one year of ISS orbit life in case of supply interruption. A Propulsion Module would have been attached to the Unity end of the ISS.
Multiple supply vehicles are required to satisfy the ISS's 7000 kg annual average propellant need. The current plan for 6 Progress M1 spacecraft per year meets that need.
The Propulsion module would hold 9808 kg fuel. Progress M holds 1100 kg; Progress M1 holds 1950 kg. ESA ATV holds 4000 kg. The cancelled U.S. Interim Control Module holds 5000 kg of fuel. A Shuttle Orbiter ISS generic reboost has 232 kg of fuel available. An Orbiter Max reboost mission has 1626 kg of reboost fuel available. Zarya FGB holds 5500 kg and the Zvezda Service module holds 860 kg, however, it is generally preferred to keep the main thrusters on Zarya and Zvezda in reserve, as they have finite lifespans.
The Propulsion module, besides being part of the backup plan for if the Service Module was not available, was intended to be an American-owned propulsion system for the station and planned as a late addition. However, the original design was overbudget and late. An alternative design, the "Node X" design, which was built around an improperly fabricated hull intended for Node 2 or 3, was then proposed and tentatively included in the plan, designed with two detachable fuel modules that could be carried up and down in a shuttle cargo bay for replacement to avoid the problems of transferring propellant between tanks in space. It has subsequently been deleted from the plans, instead requiring the station to rely on the ATV and Progress spacecraft for reboost. Furthermore, in the wake of the Shuttle's retirement, further redesign would have been necessary.
|
|
|---|
|
Already launched: Zarya | Unity (Node 1) | Zvezda | Destiny | Quest airlock | Pirs airlock Launched periodically: Multi-Purpose Logistics Module Scheduled for Shuttle: Harmony (Node 2) | Columbus | Kibō | SPDM | Node 3 | Cupola Scheduled for Proton: Multipurpose Laboratory Module | European Robotic Arm | Russian Research Module Other subsystems: Integrated Truss Structure | Canadarm2 Canceled or unused: Interim Control Module | Universal Docking Module | Docking and Stowage Module | Habitation Module | Crew Return Vehicle | Propulsion Module Ships: Soyuz | Progress | H-II Transfer Vehicle | Automated Transfer Vehicle See also: assembly sequence |
