GENESIS MISSION FACT SHEET

MISSION SUMMARY: Genesis returns solar matter for compositional analysis in terrestrial laboratories. Ultra-pure materials will be exposed to the solar wind for two years. Because the Sun comprises >99% of the mass of our solar system, average solar system isotopic and elemental compositions can be obtained. Basic feasibility was demonstrated by short (2-40 hour) exposures during Apollo.

MISSION STATUS: As Suess-Urey we have completed Phase A, producing a full Implementation Plan and Science Requirements Document. We tied for first in the Discovery 4 competition. In this proposal we have maintained our strengths (excellent in science and mission implementation; highest rating for management)), but we have worked hard to improve significantly the areas where we were weak (good for cost; fair for outreach). We are ready for Phase B.


Science Value

The highly diverse objects of our solar system originated from a relatively homogeneous solar nebula. Ultimately, the correct theories for the origins of these objects, including planetary atmospheres, will be validated by their predictions of chemical and isotopic compositions relative to the average nebular composition preserved in the surface layers of the Sun. Genesis provides solar abundances at the precision required to test these theories. Moreover, Genesis will test fundamental assumptions, such as whether or not solar and nebular compositions are identical.


Science Objectives
Highest Priority Measurements

INSTRUMENTS

Collector Arrays (JPL) High purity materials into which solar wind ions are implanted. Different arrays sample the 3 different kinds of solar wind (regimes), providing corrections for any elemental or isotopic differences between solar wind and solar abundances.

Concentrator (LANL) An electrostatic mirror concentrates (factor >20) elements up to Ne, necessary to achieve required precision for highest priority objective (O isotopes).

Monitors (LANL) Ion and electron electrostatic analyzers provide data to set concentrator voltages and to deploy appropriate array for prevailing regime.

Laboratory Analytical Instruments Genesis samples will be analyzed in Advanced Analytical Instrument Facilities, selected based on open competition and developed in Phase E.

MISSION DESCRIPTION

A spinning spacecraft will be inserted into a halo orbit about the L1 Lagrangian point (0.01 AU from Earth) where collector arrays will be exposed to the solar wind for two years, stowed into a contamination-tight canister within a Sample Return Capsule (SRC), and returned to Earth for mid-air recovery in Utah. In case of bad weather, 10 day parking orbits permit delayed entry. Allowable launch periods are very wide.


MISSION FEATURES AND BENEFITS

Samples are Returned to Earth
Simple Mission Design
Simple, Low-risk Spacecraft; Very Simple Mission Operations
Opportunity Benefits Beyond Science Return

SPACECRAFT

The Genesis spacecraft is built around a Sample Return Capsule (SRC) containing an ultra-clean canister which houses the collector arrays and concentrator. Spacecraft subsystems and monitors are mounted beneath the SRC.

 

TEAMING AND MANAGEMENT

The Genesis Team consists of Caltech (science), Lockheed Martin Astronautics (flight system), JPL (payload and management), LANL (monitors and concentrators), and JSC (contamination control and curation). Management based on Integrated Product Teams (IPT) bound by Integrated (i,e, team-wide) Systems Engineering and lean, but effective, Integrated Management. The IPTs have considerable autonomy but are constrained by overall schedule and spending profile as monitored by Project Manager.

SCHEDULE
Phase B 8 months
Phase C/D 29.5 months
Launch Jan. 2001
Recovery Aug. 2003
Phase E 2/01 - 7/07

 

 


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