JPL Technical Report Server

The plans for getting OCO-2 into orbit

Show simple item record

dc.contributor.author Vincent, Mark A.
dc.contributor.author . Garcia, Mark D
dc.date.accessioned 2013-12-11T00:25:10Z
dc.date.available 2013-12-11T00:25:10Z
dc.date.issued 2013-02-10
dc.identifier.citation 23rd AAS/AIAA Spaceflight Mechanics Meeting, Kauai, Hawaii, February 10-14 2013 en_US
dc.identifier.clearanceno 13-0774
dc.identifier.uri http://hdl.handle.net/2014/44066
dc.description.abstract The method and terms used to design the target parameters that will be used to insert the Orbiting Carbon Observatory 2 (OCO-2) into the A-train are defined. Comparisons are made to the plan that would have been used had OCO-1 successfully achieved its Injection Orbit. Major differences arise from the fact that OCO-1 was launched on a Taurus XL with a target 65 km below the A-Train while OCO-2 will be launched on a Delta II with a target only 15 km below the A-Train. The new plan is similar to the one used for the CloudSat/CALIPSO missions, but reformulated into a one-step iteration process that is easier to understand. en_US
dc.description.sponsorship NASA/JPL en_US
dc.language.iso en_US en_US
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2013 en_US
dc.subject Orbiting Carbon Observatory 2 (OCO-2) en_US
dc.subject launch vehicle en_US
dc.subject Injection Orbit en_US
dc.subject safety planning en_US
dc.subject lessons learned en_US
dc.title The plans for getting OCO-2 into orbit en_US
dc.type Preprint en_US


Files in this item

This item appears in the following Collection(s)

Show simple item record

Search


Browse

My Account