SpaceLoft-XL

SpaceLoft-XL [UP Aerospace]

The SpaceLoft-XL is a small sounding rocket developed by UP Aerospace.

The rocket has a diameter of 25 cm and a lenght of 6 m. It has the capability of lofting a 50 kg payload to a sub-orbital trajectory with an apogee of 105 km or smaller payloads up to 225 km. It is powered by a solid rocket motor with a burn time of 12 sec.

Launch site is the SouthWest Regional Spaceport (Spaceport America) in New Mexico.

Version	Stage 1
Spaceloft	Spaceloft
Spaceloft-XL	Spaceloft-XL

Nr   TNr   Vehicle            Date        LS      Sub Suc         Payload

 1     1   SpaceLoft-XL       25.09.2006  SA        * F           ? 
 2     2   SpaceLoft-XL       28.04.2007  SA        *             Celestis 06 
 3     3   SpaceLoft-XL       02.05.2009  SA        * F           Celestis 08
 4     4   SpaceLoft-XL       04.05.2010  SA        *             Celestis 09
 5     5   SpaceLoft-XL       20.05.2011  SA        *             Celestis 10 
 6     6   SpaceLoft-XL       05.04.2012  SA        *             ORS 

 
SA = Spaceport America (SouthWest Regional Spaceport), New Mexico