Sitemap | Print | Start page

SSC GroupSystems & Services Current activitiesExperiencePress roomCAREERContact
Maxus 7
Maxus 6
Maxus 5
Maxus 4
Maxus 3
Maxus 2
Maxus 1
Maxus 4

motorhigh
Motor on the launch pad.

Campaign information Maxus 4 (2001)


GENERAL INFORMATION
Launch site: Esrange Space Center
Launch window:
Launch date: 29 Apr 2001 at 13:30, local time
Customer: The Maxus program is financed by ESA and exclusively carry ESA experiments.
Purpose: The scientific objective is to perform experiments during 12-13 minutes of microgravity (10-4 g) using a single stage sounding rocket motor.
Media information Press releases, photos and/or videos are found here.

PARTICIPATING ORGANISATIONS
Funding agency: ESA
Principal investigator: Prof. Frohberg, ESA
Launch contractor: Astrium-ST and SSC
Research organizations: University of Giessen, University of Naples, CNRS Meudon, YKI Stockholm, University of Freiburg, University of Leuven
Contact persons: Mr B. Larsson, SSC Space System, Project manager
Mr B. Sjöholm, SSC Esrange, Project manager
Mr W. Herfs, Project manager, ESA
Mr B. Franke, ASTRIUM


TECHNICAL INFORMATION
Launcher: Maxus tower
Rocket motor: CASTOR 4B (ATK Thiokol Corporation, USA), see Rocket motors
Motor type: Guided singel stage
Motor length: 11 m
Motor weight: 11,6 ton (solid propellant 9,9 ton)
Burning time: 62 sec

Apogee:

703,6 km
Microgravity: 12 minutes
Rocket systems: SSC has designed and constructed the motor adapter (INA), the motor telemetry unit (TTU).
Saab Ericsson Space has developed the guidance and navigation control module (GCS).
Experiment modules: SSC developed 1 module
Astrium-ST developed 4 modules.
Payload service systems: Kayser-Threde was responsible for the service system.
Payload length: 6,48 m
Payload weight: 804 Kg

EXPERIMENT MODULES
Module Experiment Developed by Investigator
TEM
06-27M
Multi-roll Instability of Thermocapillary Flow and Transition To Oscillary Flow in Long Floating Zones. D. Schawbe, University of Giessen
TEM
06-4M

Pulsating and Rotating Instabilities in Marangoni Flows (PULSAR 2)

R. Monti, University of Naples
FOAMS Physics of Foams
Read more here.

SSC

M. Adler, CNRS Meudon
B. Kronberg, YKI Stockholm
TEM
02-5M
Application of a Rotating Magnetic Field for the Suppression of Time-dependent Maragoni Convection
T. Hibiya, S. Nakamura, NEC Japan

K. Benz, A. Cröll, P. Dold, M. Schweizer, University of Freiburg

TEM
06-26M

Crystallization of MFI type Zeolite from Clear Solution,

J. Martens, C.E. A. Kirschhock, University of Leuven.

 



© Copyright Swedish Space Corporation Email: info@ssc.se