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Example of Acta Astronautica format Example of Acta Astronautica format Example of Acta Astronautica format Example of Acta Astronautica format Example of Acta Astronautica format Example of Acta Astronautica format Example of Acta Astronautica format
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Example of Acta Astronautica format Example of Acta Astronautica format Example of Acta Astronautica format Example of Acta Astronautica format Example of Acta Astronautica format Example of Acta Astronautica format Example of Acta Astronautica format
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open access Open Access ISSN: 945765

Acta Astronautica — Template for authors

Publisher: Elsevier
Categories Rank Trend in last 3 yrs
Aerospace Engineering #14 of 129 up up by 6 ranks
journal-quality-icon Journal quality:
High
calendar-icon Last 4 years overview: 2164 Published Papers | 11596 Citations
indexed-in-icon Indexed in: Scopus
last-updated-icon Last updated: 19/07/2020
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Journal Performance & Insights

  • CiteRatio
  • SJR
  • SNIP

CiteRatio is a measure of average citations received per peer-reviewed paper published in the journal.

5.4

6% from 2019

CiteRatio for Acta Astronautica from 2016 - 2020
Year Value
2020 5.4
2019 5.1
2018 4.4
2017 3.8
2016 3.4
graph view Graph view
table view Table view

insights Insights

  • CiteRatio of this journal has increased by 6% in last years.
  • This journal’s CiteRatio is in the top 10 percentile category.

SCImago Journal Rank (SJR) measures weighted citations received by the journal. Citation weighting depends on the categories and prestige of the citing journal.

1.134

6% from 2019

SJR for Acta Astronautica from 2016 - 2020
Year Value
2020 1.134
2019 1.065
2018 0.907
2017 0.758
2016 1.009
graph view Graph view
table view Table view

insights Insights

  • SJR of this journal has increased by 6% in last years.
  • This journal’s SJR is in the top 10 percentile category.

Source Normalized Impact per Paper (SNIP) measures actual citations received relative to citations expected for the journal's category.

1.7

13% from 2019

SNIP for Acta Astronautica from 2016 - 2020
Year Value
2020 1.7
2019 1.959
2018 2.156
2017 1.886
2016 1.948
graph view Graph view
table view Table view

insights Insights

  • SNIP of this journal has decreased by 13% in last years.
  • This journal’s SNIP is in the top 10 percentile category.

Related Journals

open access Open Access ISSN: 8858985

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CiteRatio: 6.8 | SJR: 1.321 | SNIP: 1.764
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Acta Astronautica

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Elsevier

Acta Astronautica

Acta Astronautica is sponsored by the International Academy of Astronautics. Content is based on original contributions in all fields of basic, engineering, life and social space sciences and of space technology related to:  The peaceful scientific exploration of space, Its ex...... Read More

Engineering

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Last updated on
18 Jul 2020
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ISSN
0094-5765
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Impact Factor
High - 1.432
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Open Access
No
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Sherpa RoMEO Archiving Policy
Green faq
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Plagiarism Check
Available via Turnitin
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Endnote Style
Download Available
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Bibliography Name
elsarticle-num
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Citation Type
Numbered
[25]
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Bibliography Example
G. E. Blonder, M. Tinkham, T. M. Klapwijk, Transition from metallic to tunneling regimes in superconducting microconstrictions: Excess current, charge imbalance, and supercurrent conversion, Phys. Rev. B 25 (7) (1982) 4515–4532. URL 10.1103/PhysRevB.25.4515

Top papers written in this journal

Journal Article DOI: 10.1016/0094-5765(77)90096-0
Nonlinear analysis of hydrodynamic instability in laminar flames—I. Derivation of basic equations
G.I. Sivashinsky1
01 Nov 1977 - Acta Astronautica

Abstract:

An asymptotic nonlinear integrodifferential equation is derived for spontaneous instability of the plane front of a laminar flame. If the combustible mixture is deficient in the light component, spontaneous instability will lead to self-turbulization of the flame, and the flame front assumes a strongly nonstationary cellular ... An asymptotic nonlinear integrodifferential equation is derived for spontaneous instability of the plane front of a laminar flame. If the combustible mixture is deficient in the light component, spontaneous instability will lead to self-turbulization of the flame, and the flame front assumes a strongly nonstationary cellular structure. If there is an excess of the light component, spontaneous instability produces stationary, irregular wrinkles on the flame front, and the flame continues to propagate in a laminar regime. It is shown that in all cases spontaneous instability of the flame implies an increase in its propagation velocity. read more read less

Topics:

Laminar flame speed (68%)68% related to the paper, Instability (54%)54% related to the paper, Laminar flow (54%)54% related to the paper
1,159 Citations
open accessOpen access Journal Article DOI: 10.1016/0094-5765(74)90066-6
The asymptotic structure of counterflow diffusion flames for large activation energies
Amable Liñán1
01 Jul 1974 - Acta Astronautica

Abstract:

The structure of steady state diffusion flames is investigated by analyzing the mixing and chemical reaction of two opposed jets of fuel and oxidizer as a particular example. An Arrhenius one-step irreversible reaction has been considered in the realistic limit of large activation energies. The entire range of Damkohler numbe... The structure of steady state diffusion flames is investigated by analyzing the mixing and chemical reaction of two opposed jets of fuel and oxidizer as a particular example. An Arrhenius one-step irreversible reaction has been considered in the realistic limit of large activation energies. The entire range of Damkohler numbers, or ratio of characteristic diffusion and chemical times, has been covered. When the resulting maximum temperature is plotted in terms of the Damkohler number (which is inversely proportional to the flow velocity) the characteristic S curve emerges from the analysis, with segments from the curve resulting from: 1. (a) A nearly frozen ignition regime where the temperature and concentrations deviations from its frozen flow values are small. The lower branch and bend of the S curve is covered by this regime. 2. (b) A partial burning regime, where both reactants cross the reaction zone toward regions of frozen flow. This regime is unstable. 3. (c) A premixed flame regime where only one of the reactants leaks through the reaction zone, which then separates a region of frozen flow from a region of near-equilibrium. 4. (d) A near-equilibrium diffusion controlled regime, covering the upper branch of the S curve, with a thin reaction zone separating two regions of equilibrium flow. Analytical expressions are obtained, in particular, for the ignition and extinction conditions. read more read less

Topics:

Premixed flame (54%)54% related to the paper, Diffusion (business) (53%)53% related to the paper, Flow velocity (51%)51% related to the paper, Damköhler numbers (50%)50% related to the paper, Activation energy (50%)50% related to the paper
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759 Citations
Journal Article DOI: 10.1016/0094-5765(76)90105-3
Fracture mechanics of piezoelectric materials
01 Sep 1976 - Acta Astronautica

Abstract:

The paper provides an analysis of the deformation of a piezoelectric medium under mechanical stress. On this basis a rational approach is provided for the determination of critical load conditions leading to development of cracks, elucidating the mechanism of fracture. The paper provides an analysis of the deformation of a piezoelectric medium under mechanical stress. On this basis a rational approach is provided for the determination of critical load conditions leading to development of cracks, elucidating the mechanism of fracture. read more read less

Topics:

Fracture mechanics (61%)61% related to the paper, Fracture (geology) (53%)53% related to the paper
475 Citations
Journal Article DOI: 10.1016/J.ACTAASTRO.2004.05.052
Advanced ceramic matrix composite materials for current and future propulsion technology applications
S. Schmidt, Steffen Beyer, Helmut Knabe1, H. Immich, R. Meistring, A. Gessler
01 Aug 2004 - Acta Astronautica

Abstract:

Current rocket engines, due to their method of construction, the materials used and the extreme loads to which they are subjected, feature a limited number of load cycles. Various technology programmes in Europe are concerned, besides developing reliable and rugged, low cost, throwaway equipment, with preparing for future reu... Current rocket engines, due to their method of construction, the materials used and the extreme loads to which they are subjected, feature a limited number of load cycles. Various technology programmes in Europe are concerned, besides developing reliable and rugged, low cost, throwaway equipment, with preparing for future reusable propulsion technologies. One of the key roles for realizing reusable engine components is the use of modern and innovative materials. One of the key technologies which concern various engine manufacturers worldwide is the development of fibre-reinforced ceramics—ceramic matrix composites. The advantages for the developers are obvious—the low specific weight, the high specific strength over a large temperature range, and their great damage tolerance compared to monolithic ceramics make this material class extremely interesting as a construction material. Over the past years, the Astrium company (formerly DASA) has, together with various partners, worked intensively on developing components for hypersonic engines and liquid rocket propulsion systems. In the year 2000, various hot-firing tests with subscale (scale 1:5) and full-scale nozzle extensions were conducted. In this year, a further decisive milestone was achieved in the sector of small thrusters, and long-term tests served to demonstrate the extraordinary stability of the C/SiC material. Besides developing and testing radiation-cooled nozzle components and small-thruster combustion chambers, Astrium worked on the preliminary development of actively cooled structures for future reusable propulsion systems. In order to get one step nearer to this objective, the development of a new fibre composite was commenced within the framework of a regionally sponsored programme. The objective here is to create multidirectional (3D) textile structures combined with a cost-effective infiltration process. Besides material and process development, the project also encompasses the development of special metal/ceramic and ceramic/ceramic joining techniques as well as studying and verifying non destructive investigation processes for the purpose of testing components. read more read less

Topics:

Propulsion (53%)53% related to the paper
475 Citations
Journal Article DOI: 10.1016/0094-5765(77)90053-4
A unified statistical model of the premixed turbulent flame
K.N.C. Bray1, J.B. Moss1
01 Mar 1977 - Acta Astronautica

Abstract:

A unified statistical analysis of the premixed turbulent flame supported by a single-step global reaction is presented. A set of time-averaged balance equations derived from the exact equations of reacting turbulent flow under a thin shear layer, fast chemistry approximation are employed. These equations are closed at the lev... A unified statistical analysis of the premixed turbulent flame supported by a single-step global reaction is presented. A set of time-averaged balance equations derived from the exact equations of reacting turbulent flow under a thin shear layer, fast chemistry approximation are employed. These equations are closed at the level of turbulence kinetic energy and mean square fluctuation in reaction product concentration, and closure is effected by postulating that the probability density function for product concentration can be specified. The equations which emerge are capable of spanning the range from chemistry- to mixing-limited combustion. An approximate description of turbulent mixing-limited combustion is shown to lead to an explicit time-averaged reaction rate expression similar to Spalding's eddy break-up model. In restricted circumstances the concentration of a trace species which does not contribute significantly to the heat release can be incorporated into the model. Some alternative forms of the probability density function encompassing wrinkled laminar flames and distributed reaction are suggested. Their impact on both the model proposed and the statistical behaviour of experimental observables is investigated—the latter with a view to identifying those experiments which might provide the insight necessary to permit the specification of the probability density function fundamental to the present approach. read more read less

Topics:

Turbulence kinetic energy (55%)55% related to the paper, Probability density function (53%)53% related to the paper, Turbulence (52%)52% related to the paper, Reaction rate (51%)51% related to the paper, Laminar flow (50%)50% related to the paper
395 Citations
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Acta Astronautica format uses elsarticle-num citation style.

Automatically format and order your citations and bibliography in a click.

SciSpace allows imports from all reference managers like Mendeley, Zotero, Endnote, Google Scholar etc.

Frequently asked questions

Absolutely not! With our tool, you can freely write without having to focus on LaTeX. You can write your entire paper as per the Acta Astronautica guidelines and autoformat it.

Yes. The template is fully compliant as per the guidelines of this journal. Our experts at SciSpace ensure that. Also, if there's any update in the journal format guidelines, we take care of it and include that in our algorithm.

Sure. We support all the top citation styles like APA style, MLA style, Vancouver style, Harvard style, Chicago style, etc. For example, in case of this journal, when you write your paper and hit autoformat, it will automatically update your article as per the Acta Astronautica citation style.

You can avail our Free Trial for 7 days. I'm sure you'll find our features very helpful. Plus, it's quite inexpensive.

Yup. You can choose the right template, copy-paste the contents from the word doc and click on auto-format. You'll have a publish-ready paper that you can download at the end.

A matter of seconds. Besides that, our intuitive editor saves a load of your time in writing and formating your manuscript.

One little Google search can get you the Word template for any journal. However, why do you need a Word template when you can write your entire manuscript on SciSpace, autoformat it as per Acta Astronautica's guidelines and download the same in Word, PDF and LaTeX formats? Try us out!.

Absolutely! You can do it using our intuitive editor. It's very easy. If you need help, you can always contact our support team.

SciSpace is an online tool for now. We'll soon release a desktop version. You can also request (or upvote) any feature that you think might be helpful for you and the research community in the feature request section once you sign-up with us.

Sure. You can request any template and we'll have it up and running within a matter of 3 working days. You can find the request box in the Journal Gallery on the right sidebar under the heading, "Couldn't find the format you were looking for?".

After you have written and autoformatted your paper, you can download it in multiple formats, viz., PDF, Docx and LaTeX.

To be honest, the answer is NO. The impact factor is one of the many elements that determine the quality of a journal. Few of those factors the review board, rejection rates, frequency of inclusion in indexes, Eigenfactor, etc. You must assess all the factors and then take the final call.

SHERPA/RoMEO Database

We have extracted this data from Sherpa Romeo to help our researchers understand the access level of this journal. The following table indicates the level of access a journal has as per Sherpa Romeo Archiving Policy.

RoMEO Colour Archiving policy
Green Can archive pre-print and post-print or publisher's version/PDF
Blue Can archive post-print (ie final draft post-refereeing) or publisher's version/PDF
Yellow Can archive pre-print (ie pre-refereeing)
White Archiving not formally supported
FYI:
  1. Pre-prints as being the version of the paper before peer review and
  2. Post-prints as being the version of the paper after peer-review, with revisions having been made.

The 5 most common citation types in order of usage are:.

S. No. Citation Style Type
1. Author Year
2. Numbered
3. Numbered (Superscripted)
4. Author Year (Cited Pages)
5. Footnote

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After uploading your paper on SciSpace, you would see a button to request a journal submission service for Acta Astronautica.

Each submission service is completed within 4 - 5 working days.

Yes. SciSpace provides this functionality.

After signing up, you would need to import your existing references from Word or .bib file.

SciSpace would allow download of your references in Acta Astronautica Endnote style, according to elsevier guidelines.

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