| Literature DB >> 32596410 |
Inés Sanz-Morère1, Sebastian D Eastham1, Raymond L Speth1, Steven R H Barrett1.
Abstract
The radiative forcing resulting from condensation clouds behind aircraft ("contrails") has been estimated to have an effect on the same order of magnitude as all accumulated aviation-attributable CO2. However, contrail impacts are highly uncertain, with estimates of total contrail-driven forcing made in the past five years varying by a factor of 4. Two of the key driving uncertainties are the crystal shape and size, which describe the cloud optical properties. Here we combine data from high-fidelity scattering simulations of single crystals with in situ measurement of bulk contrail ice properties to bound the range of realistic optical properties for contrail ice. Accounting for the full range of measured contrail microphysical evolution pathways, and for a given estimate of contrail coverage, we find that the global net radiative forcing due to contrails in 2015 is between 8.6 and 10.7 mW/m2. Relative to the midpoint, this uncertainty range is less than one-quarter of that recently reported in the literature. This reduction in uncertainty is primarily due to the elimination of spheres as a plausible long-term shape for contrail ice, leaving questions of contrail coverage and optical depth as the primary causes of contrail forcing uncertainty.Entities:
Year: 2020 PMID: 32596410 PMCID: PMC7313655 DOI: 10.1021/acs.estlett.0c00150
Source DB: PubMed Journal: Environ Sci Technol Lett
Uncertainties Due to Crystal Shape in Various Estimates of Contrail Radiative Forcinga
| {(RFH – RFL)/[1/2(RFH + RFL)]} × 100 | |||||
|---|---|---|---|---|---|
| RFLW | RFSW | net RF | year | assumed crystal shape | |
| Meerkoter et al., 1999 | 10% | 9.5% | 18% | 1999 | spherical, hexagonal |
| Marquart et al., 2003 | – | – | 13% | 1992 | spherical, spherical modified |
| Rap et al., 2010 | 4.8% | 87% | 57% | 2002 | spherical, hexagonal, aggregates |
| Markowicz et al., 2011 | 47% | 78% | 95% | 2000 | 10 different shapes (including spherical) |
| Frömming et al., 2011 | 0% | 40% | 13% | 2000 | spherical, hexagonal |
| Schumann et al., 2012 | – | – | ∼180% | – | eight different shapes (including spherical) |
| Caiazzo et al., 2018 | – | – | 102% | 2006 | five different shapes (including spherical) |
The definition of “uncertainty range” can be found in section S1 of the Supporting Information.
Figure 1Assumed evolution for the contrail asymmetry parameter g. (a) Approximation of the microphysical evolution of contrail particles based on in situ measurements. (b) Range of evolutions assumed to be plausible (L, C, H: test cases used to evaluate uncertainty on 2015 global contrail RF). (a) The asymmetry parameter g is assumed to evolve linearly along two segments: an initial linear decrease from 0.88 over some time period ta followed by a period of fixed g. The initial state is assumed to be approximately spherical based on measurements.[12] (b) Domain of evolutions tested. Parameters defining evolution (g and ta) are assumed to be within the ranges of g = [0.75–0.79] and ta = [5–40 min]. L (low), C (central or baseline), and H (high) correspond to the three test cases explored for 2015 global contrails.