Outer Solar System spacecraft to probe the $\mu$Hz gravitational wave frontier

TL;DR

This paper proposes a novel space-based gravitational wave detector in the outer Solar System that avoids onboard test masses by utilizing low-acceleration environments, potentially enabling detection of microhertz gravitational waves.

Contribution

It introduces a new design for gravitational wave detection using spacecraft in the outer Solar System, eliminating the need for onboard test masses and leveraging low-acceleration conditions.

Findings

Spacecraft at >10 AU can achieve stochastic gravitational wave background sensitivities.

Radio transmission design can reach sensitivities at frequencies below 0.3×10^{-4} Hz.

Single-arm configurations are feasible with high-stability clocks.

Abstract

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 inter-spacecraft distances of $\gtrsim 10$ 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 $\sim 10$ Watt 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 $\sim10^4\times$ longer wavelengths, even a design with radio transmissions could reach stochastic background-limited sensitivities at $\lesssim 0.3\times 10^{-4}$ 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 $10^4$ seconds 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.