SPIDER RSS

Small Payloads for Investigation of Disturbances in Electrojet by Rockets

SPIDER is developed under the new Swedish national balloon and rocket programme. SPIDER will carry a payload of ten (10) free flying units (FFU) to be released from the main payload at ~65 km. The FFU’s will deploy probes on wire booms to measure turbulences in the auroral electrojet between 95 km and 115 km.

The research will be carried out using a single stage S30 in early winter 2016.

The payload will be launched in this period into geo-magnetically active conditions to study the auroral electrojet.
The FFU’s will be deployed from a spinning main payload and use their residual spin after deployment to extract their wire booms. All FFU’s are self-sufficient and will be recovered by helicopter for data extraction after landing with their own parachute system.

SSC is contracted for the mission

SSC is in addition providing

  • Project management
  • Service systems
  • System integration and testing
  • Launch service (Eurolaunch)
  • Operations

P.I. is Ass. Prof. Nickolay Ivchenko, Department of Space and Plasma
Physics at the Royal Institute of Technology (KTH)

The FFU’s and their ejection system are developed by KTH

General information

Launch site Esrange Space Center
Launch date First opportunity
February 1, 2016
 Funded by  SNSB

Technical information

Rocket type single stage S30
Nominal
payload diameter
14-inch

Nominal
payload mass

~ 240 kg including LEEWAVES
Apogee ~ 125 km

Contact person

Krister Sjölander, Project manager, (SSC)
krister.sjolander@sscspace.com

Mikael Töyrä, Project Manager for the launch facilities (SSC)
mikael.toyra@sscspace.com

 


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