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Journal of Spacecraft and Rockets
United States · American Institute of Aerona...
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Journal of Spacecraft and Rockets

Journal of Spacecraft and Rockets is a journal indexed in SJR in Space and Planetary Science and Aerospace Engineering with an H index of 92. It has an SJR impact factor of 0,821 and it has a best quartile of Q1. It is published in English. It has an SJR impact factor of 0,821.

Journal of Spacecraft and Rockets focuses its scope in these topics and keywords: control, blackout, interstellar, microgravity, mitigation, ultralight, antennamodeling, vehiclesrobust, constellations, variablespeed, ...

ISSN: 0022-4650
Publisher: American Institute of Aeronautics and Astronautics Inc. (AIAA)
Category: Space and Planetary Science
Indexation: verifiedScopus / SJR verifiedWeb of Science
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schedule CountryOfPapers database fields
SJR Impact Factor trending_up
0,821 Q1
H-index 92
Acceptance rate pie_chart
26% Selective
Source Acceptance_Rate
Time to publication hourglass_top
NPD
Field NPD
Publication cost (APC) payments
NPD Subscription
Non-OA path NPD

Metrics

Scimago and CountryOfPapers database fields

Scopus / SJR Web of Science

SJR Impact

0,821

H-index

92

Docs (year)

142

Docs 3y

480

Total refs

4860

Cites 3y

1172

Citable 3y

437

Cites/Doc 2y

2.34

Ref/Doc

34.23

Immediate OA

—

Embargoed OA

NPD

Non OA / Submission

—

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Best articles by citations

An improved method for accelerometer precision centrifuge test data reduction

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Use of thermal greases to conduct heat across sheetmetal interfaces.

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Comparison of Hydrogen and Hydrocarbon-Fueled Scramjet Engines for Orbital Insertion

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Comment on Special Section: New Perspectives on the Satellite Drag Environments of Earth, Mars, and Venus

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Combined Release and Radiation Effects Satellite

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Behavior of the incidence of an accelerated missile with locked controls.

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Attitude Dynamics of Satellites with Flexible Appendages- A Brief Review

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Applications of a Counterflow Drag Reduction Technique in High-Speed Systems

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Application of the line-source technique for vacuum thermal conductivity measurements

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Application of System-Identification Techniquest to Health Monitoring of On-Orbit Satellite Boom Structures

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Analysis of Two-Segment Lunar Free-Return Trajectories

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Analysis of movable louvers for temperature control

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Aerothermodynamic Testing of the Crew Exploration Vehicle at Mach 6 and Mach 10

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Aerothermodynamic Testing and Boundary-Layer Trip Sizing of the HIFiRE Flight 1 Vehicle

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Aeroheating Testing and Predictions for Project Orion Crew Exploration Vehicle

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Aerodynamic Characterization of a Microspoiler System for Supersonic Finned Projectiles

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