The DS defined GEO-CAPE as a Tier 2 mission that could be implemented with mature instrumentation that had significant space heritage in LEO. The implied mission implementation was multiple instruments on one large spacecraft. Although this implementation approach for GEO-CAPE was studied and found to be technically feasible, the total cost of a single large mission appears to be prohibitively expensive. Consequently, alternative mission implementation concepts [PDF] that would launch individual GEO-CAPE instruments on separate spacecraft are being studied to provide flexibility while reducing cost and risk.
Ongoing studies continue to refine GEO-CAPE measurement and instrument requirements. Specific instruments for GEO-CAPE have not yet been selected. A conceptual planning payload based on the notional instruments described in the Decadal Survey is being used to advance the mission design studies. + View the GEO-CAPE Planning Payload Document [PDF]
At this preliminary stage, several instrument concepts are being studied to ensure that a range of potential instruments can meet GEO-CAPE atmosphere and ocean requirements. These instrument concepts are suitable for implementation either together on a single dedicated satellite or individually as secondary payloads on separate spacecraft.
Instrumentation hosted as secondary payloads on commercial satellite missions offers several benefits that can reduce mission implementation cost and risk.
The goal of these alternative concepts is to allow all of the scientific objectives of GEO-CAPE to be accomplished sooner than otherwise possible. A notional timeline shows how individual components of GEO-CAPE could be aligned with complementary US and international missions.