Geometry & materials

Nanophotonic Heterostructures for Efficient Propulsion and Radiative Cooling of Relativistic Light Sails

2018 · Published theoretical design study

Theory & models

What this work contributes

Compares thin-film structures for low laser absorption, useful reflectivity, low areal mass and infrared heat rejection. A proposed figure of merit exposes the trade-off between reflectivity and sail mass rather than optimizing reflectivity alone.

Where the evidence stops

These are calculated materials designs. Their optical and thermal targets do not establish fabricated-sail survival, stable acceleration or flight performance.

Keep the conditions with the result

Measured / modeled quantity
Calculated reflectivity, absorptivity, emissivity and reflectivity-adjusted areal density
Reported scale
Relativistic-sail design context uses near-infrared intensities of order MW/cm²; not a measured operating rating.
Conditions
Modeled externally laser-illuminated thin-film sail with radiative cooling.
Evidence context
Theoretical comparison; an experimental reproduction is not reported in the reviewed abstract.
Design use
Link sail momentum calculations to absorption, thermal emission and total moving mass.
Review access
Publisher and institutional records compared; full main article not reviewed.

Original source

Ognjen Ilic, Cora M. Went, Harry A. Atwater. Nanophotonic Heterostructures for Efficient Propulsion and Radiative Cooling of Relativistic Light Sails. Nano Letters 18(9), 5583–5589 (2018).

DOI: 10.1021/acs.nanolett.8b02035

How we use it

This record belongs to Geometry & materials. Its evidence label describes the cited work, not the maturity of a Metric Flight device. Follow the original methods, corrections and conditions before transferring a result to a different geometry or scale.

Editorial note reviewed 19 October 2026. AI assisted research discovery and synthesis. Citation metadata and claims were checked against primary publication or institutional records; full-text access varies. Read the source for the complete method.