Central Tube: Alcatel/SAAB

STATUS | Ongoing
STATUS DATE | 16/09/2008
ACTIVITY CODE |

Objectives

This project is devoted to the pre-development of Alphabus Central Tube (@CT), equipment which belongs to the structure subsystem of the Alphabus spacecraft. This pre-development consists in demonstrating through theoretical studies and samples manufacturing that the next spacecraft generation could benefit from new technological or industrial improvements, i.e.:

  • Improved Launcher Junction Frame (LJF) design
  • LJF to shell junction (without monolithic heel)
  • Lay-up with laser projection
  • Less stringent surface treatments on inserts
  • Risk mitigation on shape defects after curing&

Challenges

The issues can be divided in design and manufacturing issues:

 

Main design issues

  • choice of the fiber wrt stiffness and mass analyses
  • prediction of deformations of the tube after curing
  • LJF design evolutions to insure load transfer between LJF and shell (which impact the tube diameter)
  • To lower cost, mass and lay-up time of the junction between LJF and shell

 

Main manufacturing issues

  • Feasibility or not to use a less impregnated prepreg technique for M55J to lower porosity in laminates
  • Study of an alternative curing process to lower porosity and have better aligned fiber in laminates
  • Study of a new method for corner manufacturing

Plan

The expected project plan is built in 3 steps as follows:


 

Current Status

Phase 1 of this pre-development has been completed with the Technology Evaluation Review held beginning of 2005.

 

The main results of the Phase 1 studies are:

  • A possibility to fix the cylinder shell to the Lower Junction Frame (LJF) with blind bolts is identified to reduce mass and optimize production time.
  • The Launcher Junction Frame (LJF) design has been studied, in order to balance the stresses in the inner and outer skins of the sandwich cylinder.
  • Shape prediction analyses have been performed to envisage tolerance compliance after cylinder curing.
  • Specific layup designs have been identified for optimization of the composite shell geometric tolerances after curing.
  • The interest for a method of hand lay-up in combination with laser projected positioning of pre-preg patches, has been investigated.
  • The Central Tube preliminary design has been established with EAR / ITAR free materials and suppliers.
  • A preliminary concept baseline and production philosophy has been defined. All necessary processes and procedures are established and validated.