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Outer Solar System Spacecraft to Probe the μHz Gravitational-wave Frontier
by
McGrath, Casey
, McQuinn, Matthew
in
Black holes
/ Doppler tracking
/ Frequencies
/ Gravitational waves
/ Interferometry
/ Isolation systems
/ Laser beams
/ Outer solar system
/ Radio transmission
/ Radio transmissions
/ Radio waves
/ Sensitivity
/ Solar system
/ Spacecraft
/ Spacecraft design
/ Supermassive black holes
/ Wavelengths
2025
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Outer Solar System Spacecraft to Probe the μHz Gravitational-wave Frontier
by
McGrath, Casey
, McQuinn, Matthew
in
Black holes
/ Doppler tracking
/ Frequencies
/ Gravitational waves
/ Interferometry
/ Isolation systems
/ Laser beams
/ Outer solar system
/ Radio transmission
/ Radio transmissions
/ Radio waves
/ Sensitivity
/ Solar system
/ Spacecraft
/ Spacecraft design
/ Supermassive black holes
/ Wavelengths
2025
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Do you wish to request the book?
Outer Solar System Spacecraft to Probe the μHz Gravitational-wave Frontier
by
McGrath, Casey
, McQuinn, Matthew
in
Black holes
/ Doppler tracking
/ Frequencies
/ Gravitational waves
/ Interferometry
/ Isolation systems
/ Laser beams
/ Outer solar system
/ Radio transmission
/ Radio transmissions
/ Radio waves
/ Sensitivity
/ Solar system
/ Spacecraft
/ Spacecraft design
/ Supermassive black holes
/ Wavelengths
2025
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Outer Solar System Spacecraft to Probe the μHz Gravitational-wave Frontier
Journal Article
Outer Solar System Spacecraft to Probe the μHz Gravitational-wave Frontier
2025
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Overview
The microhertz frequency band of gravitational waves probes the merger of supermassive black holes, as well as many other gravitational-wave phenomena. However, space-interferometry methods that use test masses would require further development of test-mass isolation systems to detect anticipated astrophysical events. We propose an approach that avoids onboard inertial test masses by situating spacecraft in the low-acceleration environment of the outer solar system. We show that, for Earth–spacecraft and interspacecraft distances of ≳10 au, the accelerations on the spacecraft would be sufficiently small to potentially achieve gravitational-wave sensitivities determined by stochastic gravitational-wave backgrounds. We further argue, for arm lengths of 10−30 au and ∼10 W transmissions, that stable phase locks could be achieved with 20 cm mirrors or 5 m radio dishes. We discuss designs that send both laser beams and radio waves between the spacecraft, finding that, despite the ∼ 104× longer wavelengths, even a design with radio transmissions could reach stochastic background-limited sensitivities at ≲0.3 × 10−4 Hz. Operating in the radio significantly reduces many spacecraft design tolerances. Our baseline concepts require two arms to do interferometry. However, if one spacecraft carries a clock with Allan deviations at 104 s of 10−17, a comparable sensitivity could be achieved with a single arm. Finally, we discuss the feasibility of achieving similar gravitational-wave sensitivities in a “Doppler tracking” configuration where the single arm is anchored to Earth.
Publisher
IOP Publishing
Subject
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