Space modules of Phobos-Grunt complex for prospective interplanetary stations

Polishchuk, G. M.; Pichkhadze, K. M.; Efanov, V. V.; Martynov, M. B.

doi:10.1134/s0038094611070252

Cited by 15 publications

(3 citation statements)

References 0 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…The search for the Sun is carried out, and the longitudinal axis is brought to it. 6. A speed impulse of 20 m/s is emitted to the propultion system of the RV in the direction of the Sun, after which the RV is in the intermediate orbit, hereinafter referred to as take-off, which touches the Phobos orbit at the take-off point and is 300-350 km away from it at the opposite point.…”

Section: Return To Earth 221 Start From Phobosmentioning

confidence: 99%

Development of the Propulsion Construction and the Trajectory of the Spacecrafts for the Study of Martian Planetary System

Platov¹,

Simonov²,

Vorobyev³

et al. 2019

SJST

View full text Add to dashboard Cite

The article provides a brief description of the flight scheme of a prospective automatic spacecraft intended for the study of Mars and its satellites by remote and contact methods. At the near-Martian expedition site, it is planned to first bring the vehicle into orbit of the artificial satellite Deimos, and then landing on Phobos with the subsequent delivery of its soil to Earth. The main ballistic characteristics of the spacecraft flight conditions at all stages of the flight at launch after 2025 are given. The time frames for the five starting periods are considered -

show abstract

Section: Return To Earth 221 Start From Phobosmentioning

confidence: 99%

Development of the Propulsion Construction and the Trajectory of the Spacecrafts for the Study of Martian Planetary System

Platov¹,

Simonov²,

Vorobyev³

et al. 2019

SJST

View full text Add to dashboard Cite

show abstract

“…In particular, this is how the "Moon" and "Phobos" (1988) programs were imple mented (Dem'yanenko et al, 1994;Polishchuk et al, 2009;Khartov et al, 2010;Pichkhadze et al, 2010;). However, the double launch of SCs in the "Phobos" project and the absence of additional goals could not compensate for the failure of the project as a whole.…”

Section: On the Implementation Of The Integrated "Apophis Boomerang" mentioning

confidence: 99%

On the implementation of the program for exploration of Solar System small bodies

et al. 2014

Self Cite

View full text Add to dashboard Cite

The paper discusses two missions for studies of various typical Solar System small bodies. The first mission is intended to study the Martian satellites and will be completed by delivering soil samples to the Earth; the second will perform a comprehensive study of a small asteroid body and deliver a radio beacon to the latter. The similarity of the technological base for both missions that enables the use of a unified design baseline is analyzed. It is suggested that the missions be joined into an integrated program consisting of two stages and that their optimal sequence order be determined.

show abstract

“…A number of space systems designed for Mars exploration contain descent vehicles (DV) to deliver a payload to the surface of the planet (Polishchuk et al, 2006;2009;. During the DV design, consider able attention is paid to the choice of its shape, deter mination of its aerodynamic properties, heat load, and structural parameters of thermal protection, which ensure a DV safe entry, as well as the prediction of its landing site.…”

Section: Introductionmentioning

confidence: 99%

Aerodynamic design of a descent vehicle in the Martian atmosphere under the exomars project

Golomazov

Finchenko

2014

Sol Syst Res

View full text Add to dashboard Cite

The paper considers mathematical support for calculation of the aerodynamics and flight trajec tory of descent vehicles (DV) during entry into the Martian atmosphere. The study of aerodynamics of a seg mental and conical DV is given under various reentry conditions. The paper presents comparison of compu tational results of the aerodynamic properties of the DV of the ExoMars project with wind tunnel test data of DV models.

show abstract

Space modules of Phobos-Grunt complex for prospective interplanetary stations

Cited by 15 publications

References 0 publications

Development of the Propulsion Construction and the Trajectory of the Spacecrafts for the Study of Martian Planetary System

Development of the Propulsion Construction and the Trajectory of the Spacecrafts for the Study of Martian Planetary System

On the implementation of the program for exploration of Solar System small bodies

Aerodynamic design of a descent vehicle in the Martian atmosphere under the exomars project

Contact Info

Product

Resources

About