QuakeFinder - Earthquake Research

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QuakeFinder can develop custom magnetometer products for your space applications
ULF/VLF/Payload
QuakeSat-2 Instrument Specs
The second generation of the QuakeSat series is being designed and built with a projected launch date of 2008. QuakeFinder at this time is actively seeking sponsors looking to integrate its payload on a satellite vehicle and deliver it into orbit.
QuakeFinder is also developing customized payload integration partnerships to be built and delivered to your specifications.
TURN KEY Sat. System
We specialize in creating low-cost solutions to your requirements. These include micro-sats (30-100kg) and nanosats (1-30 kg) which can be designed to maximize the use of commercial off-the-shelf (COTS) technologies and low cost launches from foreign as well as domestic launch providers.

QuakeSat-I
QuakeSat is a small satellite, 4”x4”x12”, launched on June 30, 2003, and provides a “proof-of-concept” for collecting ULF earthquake precursor signals from space. The design was based on the CubeSat concept where each CubeSat is 4”x4”x4”. QuakeSat is in fact a triple CubeSat to provide a large enough size to include a one-foot long magnetometer that extends on a telescoping boom.

The satellite was built by the Space Systems Development Laboratory at Stanford University, under the direction of Professor Robert Twiggs, with the receiver unit provided by QuakeFinder.
For more information on QuakeSat-I

View our Technical Papers

Download the, "QuakeSat Lessons Learned" PDF Document

Download the PDF, "A CubeSat Derived Design..."

Read the QuakeStat-1 Specs.

View the Stanford/QuakeSat Webpage

QuakeSat-II National Representation

150 kg class Microsatellite with 4 instruments (B field, E Field, Langmuir probe, Ion Detector)
Illustration courtesy of MicroSat Systems Inc (MSI)
(Ref QuakeSat I two year development cycle from concept to successful launch, and its 2 year successful on-orbit operations).
We can help you with custom applications, including all the system engineering aspects:

Mission requirements
Budget estimations
Program schedules
Requirements/Specifications/Interface Definitions
Launch options
Design
Development
Test
Calibration
Launch operations
Flight Operations/health and status
Mission Planning
Mission Data Collection/Processing
Flight Data Analyses and mission reporting

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Space Products [ User Login ][ Sign-up ]
	QuakeFinder can develop custom magnetometer products for your space applications ULF/VLF/Payload QuakeSat-2 Instrument Specs The second generation of the QuakeSat series is being designed and built with a projected launch date of 2008. QuakeFinder at this time is actively seeking sponsors looking to integrate its payload on a satellite vehicle and deliver it into orbit. QuakeFinder is also developing customized payload integration partnerships to be built and delivered to your specifications. TURN KEY Sat. System We specialize in creating low-cost solutions to your requirements. These include micro-sats (30-100kg) and nanosats (1-30 kg) which can be designed to maximize the use of commercial off-the-shelf (COTS) technologies and low cost launches from foreign as well as domestic launch providers. QuakeSat-I QuakeSat is a small satellite, 4”x4”x12”, launched on June 30, 2003, and provides a “proof-of-concept” for collecting ULF earthquake precursor signals from space. The design was based on the CubeSat concept where each CubeSat is 4”x4”x4”. QuakeSat is in fact a triple CubeSat to provide a large enough size to include a one-foot long magnetometer that extends on a telescoping boom. The satellite was built by the Space Systems Development Laboratory at Stanford University, under the direction of Professor Robert Twiggs, with the receiver unit provided by QuakeFinder. For more information on QuakeSat-I View our Technical Papers Download the, "QuakeSat Lessons Learned" PDF Document Download the PDF, "A CubeSat Derived Design..." Read the QuakeStat-1 Specs. View the Stanford/QuakeSat Webpage QuakeSat-II National Representation 150 kg class Microsatellite with 4 instruments (B field, E Field, Langmuir probe, Ion Detector) Illustration courtesy of MicroSat Systems Inc (MSI) (Ref QuakeSat I two year development cycle from concept to successful launch, and its 2 year successful on-orbit operations). We can help you with custom applications, including all the system engineering aspects: Mission requirements Budget estimations Program schedules Requirements/Specifications/Interface Definitions Launch options Design Development Test Calibration Launch operations Flight Operations/health and status Mission Planning Mission Data Collection/Processing Flight Data Analyses and mission reporting