LARES Support System

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LARES Support System

Remained attached to the AVUM upper stage. Included extensive instrumentation to monitor the launch vehicle during ascent. It also deployed seven 1U Cubesats from three P-POD deployers

Status: Operational 2012. First Launch: 2012-02-13. Last Launch: 2012-02-13. Number: 1 . Gross mass: 300 kg (660 lb). Apogee: 1,394 km (866 mi).

Subtopics

LARES-A& Null

H/SS Null

Family: Technology. Country: Europe. Launch Vehicles: Vega. Launch Sites: Kourou ELV.

LARES Support System - . Mass: 300 kg (660 lb). Nation: Europe. Class: Technology. Type: Technology satellite. Spacecraft: LARES Support System. Decay Date: 2016-11-02 . USAF Sat Cat: 38086 . COSPAR: 2012-006K. Apogee: 1,394 km (866 mi). Perigee: 270 km (160 mi). Inclination: 69.50 deg. Period: 101.50 min. Remained attached to the AVUM upper stage. Included extensive instrumentation to monitor the launch vehicle during ascent. It also deployed seven 1U Cubesats from three P-POD deployers.

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