OSIRIS-REx (New Frontiers 3)

USA

Int. spacecraft nº:

US spacecraft nº:


Launch data:

Designation 41757 / 16055A
Launch date 08 Sep 2016 - 23:05 UT
Launch site CC, SLC41
Launch vehicle  Atlas-V 411
Mission Asteroid sample return
Heliocentric orbit:
Perigee / Apogee 203 x -40174 km
Eccentricity 
Inclination  29.5°
Period  min


Spacecraft data:

Prime manufacturer Lockheed Martin Space Systems, Denver
Platform 
Operator University of Arizona for NASA
Mass at launch  1528 kg
Dry Mass  kg
Basic shape  
Dimension (m) 
Equipment Reentry capsule
Solar array 
Stabilization  
Propulsion 
DC power  
Design lifetime  + 7 yrs

Credit: OSIRIS-REX



Description:

Mission details:

External links:


Ref.: #7(JR730,741,756-759,777), #14, #127, #www.asteroidmission.org - update: 23.05.21 Home