2017
DOI: 10.2514/1.d0045
|View full text |Cite
|
Sign up to set email alerts
|

Cost-Benefit Assessment of Climate-Restricted Airspaces as an Interim Climate Mitigation Option

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

1
14
0

Year Published

2018
2018
2024
2024

Publication Types

Select...
6
2
1

Relationship

0
9

Authors

Journals

citations
Cited by 15 publications
(15 citation statements)
references
References 19 publications
1
14
0
Order By: Relevance
“…The minimum climate impact trajectories, on average, reduced ATR100 by 28.4 % with an additional COC of 7.1 %, compared to those measures of the minimum COC trajectories. Our results agree with those shown by Niklaß et al (2017).…”
Section: Characteristics Of Aircraft Routing Optionssupporting
confidence: 94%
See 1 more Smart Citation
“…The minimum climate impact trajectories, on average, reduced ATR100 by 28.4 % with an additional COC of 7.1 %, compared to those measures of the minimum COC trajectories. Our results agree with those shown by Niklaß et al (2017).…”
Section: Characteristics Of Aircraft Routing Optionssupporting
confidence: 94%
“…1). Moreover, Niklaß et al (2017) over 100 years (ATR100) and on COC under ISA conditions. They showed a clear trade-off between the cost and the climate impact.…”
Section: Characteristics Of Aircraft Routing Optionsmentioning
confidence: 99%
“…We multiply the contrail cirrus CCF by a typical specific range value for transatlantic flights of 0.16 km per kilogram of fuel (Graver andRutherford, 2018, andFlorian Linke, Deutsches Zentrum für Luftund Raumfahrt, DLR, personal communication, 2020). Similarly, the total NO x CCF is converted using a typical emissions index of NO x of 13 g NO 2 per kilogram of fuel (Penner et al, 1999). Figure 16 shows the merged CCFs of contrail cirrus, total NO x , and H 2 O exemplarily for weather situation S2 at 250 hPa and 12:00 UTC.…”
Section: Frömming Et Al: React4c Climate Change Functionsmentioning
confidence: 99%
“…S3 in the Supplement). According to Nuic et al (2010), BADA 3 has a tendency to underestimate aircraft fuel consumption at high altitudes and Mach numbers as the compressibility effect and wave drag are not modeled. These effects will cause differences in the selection of the flight altitudes.…”
Section: Optimized Flight Trajectories and Global Fieldsmentioning
confidence: 99%