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Satellite propulsion systems analysis and simulation tools.

Tools developed by Astrium's Lampoldshausen team to support satellite propulsion systems design, engineering and simulation.

 

Satellite Propulsion System Engineering & Simulation
Within the field of satellite propulsion systems, the responsibilities of Astrium's Lampoldshausen facility, near Stuttgart, Germany, extends from design, engineering, analysis and integration, through to actual hot-fire testing, test support, post-test analysis and evaluation. Most of these activities are supported by satellite propulsion system simulation tools. The performance prediction accuracy of these tools is constantly verified by actual hot-fire testing - performed within a short walk from where the tools are actually developed.
The tools developed at Lampoldshausen are used for monopropellant, bipropellant and ion thruster propulsion systems - which are also designed and developed at the same facility.

 

Software Simulation Tools
The software simulation tools developed at Lampoldshausen are not only used for satellite propulsion systems, but also interplanetary space probes, platforms, carriers, launch vehicle roll control systems, upper stage attitude and orbital control systems, and more recently for the propulsion system of the Automated Transfer Vehicle (ATV) which will be used for resupplying the International Space Station. All of these tools are precisely tailored to the specific application and customer requirements.



Historic Achievements
The historic achievements in both satellite propulsion systems and space probe propulsion systems attributed to the Lampoldshausen team include:

Symphonie
Dec 1974

TV Sat
Nov 1987

Hipparcos
Aug 1989

Galileo
Oct 1989

Symphonie satellite propulsion system TV Sat 1 satellite propulsion system Hipparcos propulsion system Galileo propulsion system

Click on images
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Recent Achievements

The first ion thruster developed in Europe used on the Artemis communications satellite.

Artemis ion thruster
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A more recent achievement attributed to the Lampoldshausen team was the development of the first ion propulsion system in Europe.

In 2001, this ion propulsion system was integrated to the Artemis telecommunications satellite as a redundant satellite propulsion system. Due to an upper stage malfunction, Artemis was injected into a low elliptical orbit with the threat of a lost mission. However, the redundant ion propulsion system was called into service and succeeded in raising Artemis into a circular 32,000 km orbit in January 2003, thereby allowing the communications satellite the possibility to operate for its nominal 10-year life.


Simulation Tools
Description
As a part of Lampoldshausen's engineering tasks, major simulation software tools have been developed to support satellite propulsion systems design, engineering and orbital operations. These tools are used in support of propulsion systems for satellites, orbital vehicles, interplanetary spacecraft, probes as well as more complex systems such as used on the Automated Transfer Vehicle (ATV

Automated Transfer Vehicle approaching the International Space Station.

ATV
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The ATV is an automated vehicle designed to transport cargo to the International Space Station (ISS). It will also be used to provide thrust for maintaining the ISS on its nominal orbit every 1.5 years. The ATV is launched into its initial orbit by Ariane 5.

ATV propulsion system testing at Lampoldshausen
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Video of ATV propulsion system testing at the P2 test facility, Lampoldshausen.
MPG movie clip, 13 sec, 2.19 MB

 

 

 

UPS Performance Analysis & Simulation Tool (UPSAT)

Flowchart UPSAT
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UPSAT (UPS Performance Analysis & Simulation Tool) is a propulsion system simulation and performance prediction tool for Unified Propulsion Systems used for satellites and space probes. UPSAT is used for all monopropellant and bipropellant propulsion systems. This fast and easy to use tool can be used with varying accuracy, depending on the nature of the task. The user can select from several component models of differing accuracy and complexity. Thus, rough but fast design computations can be performed, as well as precise performance predictions of propulsion system during orbital operations.

The range of UPSAT application extends from support to propulsion system analyses to simulation of Propulsion System main LAE operation phase (LEOP). UPSAT also gives performance predictions of LAE (Thrust, Isp, mass flow), regulated tank pressures and lock-up pressures during orbital operations.

 

ATV Propulsion System Simulation Software (ATVSim)

ATV Propulsion system schematic

Flow Schematic
ATV Propulsion System
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ATVSim (ATV Propulsion System Simulation Software) is a software tool that simulates the entire propulsion system of the ATV.

The ATV propulsion system comprises 4 x 490 N main engines and 28 x 200 N attitude control thrusters. This precision propulsion system is designed to perform orbit raising, orbital manoeuvres for ISS rendezvous and precision manoeuvres for gentle docking with the station.

Because of its close proximity with manned operations, the bi-propellant propulsion system has a high level of redundancy. Due to this redundancy, flow paths having different flow characteristics are possible during operation, depending on the status of the propellant latch valves. Consequently, the complete subsystem was modelled for compatibility with the accuracy needs.

ATVSim for modelling the ATV propulsion system

ATVSim showing selected system parameters and indicating the valve status
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ATVSim models the complete ATV propulsion system and features complex time dependant mission files for all combinations of valve status. It can define environmental temperatures and specify main engine and thruster firing duration's via a graphical user interface.

ATVSim was focused on an easy user interface with comfortable post-processing capabilities, e.g. parameters can be displayed as curves vs. time or in the form of freely definable display windows within the flow chart of the system. Here, the parameters are updated during the running of a simulation.

Due to processor advances and a deep integration within the operation system, a simulation process can be achieved, significantly faster than real-time. Even so, the software can be run on a simple laptop computer, thereby allowing portable use within an operation centre for the production of accurate and reliable flight predictions.

 

Contact for Further Information


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