Lessons learned from REXUS12'S Suaineadh Experiment: Spinning deployment of a space web in milli gravity

Thomas Sinn, Malcolm McRobb, Adam Wujek, Jerker Skogby, Fredrik Rogberg, Junyi Wang, Massimiliano Vasile, Gunnar Tibert

Research output: Contribution to conferencePaper

3 Citations (Scopus)

Abstract

On the 19th of March 2012, the Suaineadh experiment was launched onboard the sounding rocket REXUS 12 (Rocket Experiments for University Students) from the Swedish launch base ESRANGE in Kiruna. The Suaineadh experiment served as a technology demonstrator for a space web deployed by a spinning assembly. Following launch, the experiment was ejected from the ejection barrel located within the nosecone of the rocket. Centrifugal forces acting upon the space web spinning assembly were used to stabilise the experiment’s platform. A specifically designed spinning reaction wheel, with an active control method, was used. Once the experiment’s motion was controlled, a 2 m by 2 m space web is released. Four daughter sections situated in the corners of the square web served as masses to stabilise the web due to the centrifugal forces acting on them. The four daughter sections contained inertial measurement units (IMUs). After the launch of REXUS12, the recovery helicopter was unable to locate the ejected experiment, but 22 pictures were received over the wireless connection between the experiment and the rocket. The last received picture was taken at the commencement of web deployment. Inspection of these pictures allowed the assumption that the experiment was fully functional after ejection, but probably through tumbling of either the experiment or the rocket, the wireless connection was interrupted. A recovery mission in the middle of August was only able to find the REXUS12 motor and the payload impact location.

Conference

Conference21st ESA Symposium on European Rocket and balloon Programmes and Related Research
CountrySwitzerland
CityThun
Period9/06/1313/06/13

Fingerprint

Gravitation
Rockets
Experiments
Sounding rockets
Barreling
Recovery
Units of measurement
Helicopters
Wheels
Inspection
Students

Keywords

  • REXUS12
  • Suaineadh Space Web Experiment
  • milli gravity
  • spinning space web

Cite this

Sinn, T., McRobb, M., Wujek, A., Skogby, J., Rogberg, F., Wang, J., ... Tibert, G. (2013). Lessons learned from REXUS12'S Suaineadh Experiment: Spinning deployment of a space web in milli gravity. Paper presented at 21st ESA Symposium on European Rocket and balloon Programmes and Related Research, Thun, Switzerland.
Sinn, Thomas ; McRobb, Malcolm ; Wujek, Adam ; Skogby, Jerker ; Rogberg, Fredrik ; Wang, Junyi ; Vasile, Massimiliano ; Tibert, Gunnar. / Lessons learned from REXUS12'S Suaineadh Experiment : Spinning deployment of a space web in milli gravity. Paper presented at 21st ESA Symposium on European Rocket and balloon Programmes and Related Research, Thun, Switzerland.10 p.
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abstract = "On the 19th of March 2012, the Suaineadh experiment was launched onboard the sounding rocket REXUS 12 (Rocket Experiments for University Students) from the Swedish launch base ESRANGE in Kiruna. The Suaineadh experiment served as a technology demonstrator for a space web deployed by a spinning assembly. Following launch, the experiment was ejected from the ejection barrel located within the nosecone of the rocket. Centrifugal forces acting upon the space web spinning assembly were used to stabilise the experiment’s platform. A specifically designed spinning reaction wheel, with an active control method, was used. Once the experiment’s motion was controlled, a 2 m by 2 m space web is released. Four daughter sections situated in the corners of the square web served as masses to stabilise the web due to the centrifugal forces acting on them. The four daughter sections contained inertial measurement units (IMUs). After the launch of REXUS12, the recovery helicopter was unable to locate the ejected experiment, but 22 pictures were received over the wireless connection between the experiment and the rocket. The last received picture was taken at the commencement of web deployment. Inspection of these pictures allowed the assumption that the experiment was fully functional after ejection, but probably through tumbling of either the experiment or the rocket, the wireless connection was interrupted. A recovery mission in the middle of August was only able to find the REXUS12 motor and the payload impact location.",
keywords = "REXUS12, Suaineadh Space Web Experiment, milli gravity, spinning space web",
author = "Thomas Sinn and Malcolm McRobb and Adam Wujek and Jerker Skogby and Fredrik Rogberg and Junyi Wang and Massimiliano Vasile and Gunnar Tibert",
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Sinn, T, McRobb, M, Wujek, A, Skogby, J, Rogberg, F, Wang, J, Vasile, M & Tibert, G 2013, 'Lessons learned from REXUS12'S Suaineadh Experiment: Spinning deployment of a space web in milli gravity' Paper presented at 21st ESA Symposium on European Rocket and balloon Programmes and Related Research, Thun, Switzerland, 9/06/13 - 13/06/13, .

Lessons learned from REXUS12'S Suaineadh Experiment : Spinning deployment of a space web in milli gravity. / Sinn, Thomas; McRobb, Malcolm ; Wujek, Adam; Skogby, Jerker; Rogberg, Fredrik; Wang, Junyi; Vasile, Massimiliano; Tibert, Gunnar.

2013. Paper presented at 21st ESA Symposium on European Rocket and balloon Programmes and Related Research, Thun, Switzerland.

Research output: Contribution to conferencePaper

TY - CONF

T1 - Lessons learned from REXUS12'S Suaineadh Experiment

T2 - Spinning deployment of a space web in milli gravity

AU - Sinn, Thomas

AU - McRobb, Malcolm

AU - Wujek, Adam

AU - Skogby, Jerker

AU - Rogberg, Fredrik

AU - Wang, Junyi

AU - Vasile, Massimiliano

AU - Tibert, Gunnar

PY - 2013/6/16

Y1 - 2013/6/16

N2 - On the 19th of March 2012, the Suaineadh experiment was launched onboard the sounding rocket REXUS 12 (Rocket Experiments for University Students) from the Swedish launch base ESRANGE in Kiruna. The Suaineadh experiment served as a technology demonstrator for a space web deployed by a spinning assembly. Following launch, the experiment was ejected from the ejection barrel located within the nosecone of the rocket. Centrifugal forces acting upon the space web spinning assembly were used to stabilise the experiment’s platform. A specifically designed spinning reaction wheel, with an active control method, was used. Once the experiment’s motion was controlled, a 2 m by 2 m space web is released. Four daughter sections situated in the corners of the square web served as masses to stabilise the web due to the centrifugal forces acting on them. The four daughter sections contained inertial measurement units (IMUs). After the launch of REXUS12, the recovery helicopter was unable to locate the ejected experiment, but 22 pictures were received over the wireless connection between the experiment and the rocket. The last received picture was taken at the commencement of web deployment. Inspection of these pictures allowed the assumption that the experiment was fully functional after ejection, but probably through tumbling of either the experiment or the rocket, the wireless connection was interrupted. A recovery mission in the middle of August was only able to find the REXUS12 motor and the payload impact location.

AB - On the 19th of March 2012, the Suaineadh experiment was launched onboard the sounding rocket REXUS 12 (Rocket Experiments for University Students) from the Swedish launch base ESRANGE in Kiruna. The Suaineadh experiment served as a technology demonstrator for a space web deployed by a spinning assembly. Following launch, the experiment was ejected from the ejection barrel located within the nosecone of the rocket. Centrifugal forces acting upon the space web spinning assembly were used to stabilise the experiment’s platform. A specifically designed spinning reaction wheel, with an active control method, was used. Once the experiment’s motion was controlled, a 2 m by 2 m space web is released. Four daughter sections situated in the corners of the square web served as masses to stabilise the web due to the centrifugal forces acting on them. The four daughter sections contained inertial measurement units (IMUs). After the launch of REXUS12, the recovery helicopter was unable to locate the ejected experiment, but 22 pictures were received over the wireless connection between the experiment and the rocket. The last received picture was taken at the commencement of web deployment. Inspection of these pictures allowed the assumption that the experiment was fully functional after ejection, but probably through tumbling of either the experiment or the rocket, the wireless connection was interrupted. A recovery mission in the middle of August was only able to find the REXUS12 motor and the payload impact location.

KW - REXUS12

KW - Suaineadh Space Web Experiment

KW - milli gravity

KW - spinning space web

UR - http://www.spaceflight.esa.int/pac-symposium2013/

M3 - Paper

ER -

Sinn T, McRobb M, Wujek A, Skogby J, Rogberg F, Wang J et al. Lessons learned from REXUS12'S Suaineadh Experiment: Spinning deployment of a space web in milli gravity. 2013. Paper presented at 21st ESA Symposium on European Rocket and balloon Programmes and Related Research, Thun, Switzerland.