Venera-D (Russian: Венера-Д, pronounced [vʲɪˈnʲɛrə ˈdɛ]) is a proposed Russian space mission to Venus that would include an orbiter and a lander to be launched in 2031.[3] The orbiter's prime objective is to perform observations with the use of a radar. The lander, based on the Venera design, would be capable of operating for a long duration (≈3 h)[2] on the planet's surface. The "D" in Venera-D stands for "dolgozhivuschaya," which means "long lasting" in Russian.[7]
 Artist's concept of the Venera-D spacecraft approaching a cloud-veiled Venus | |
| Names | Venera 17 |
|---|---|
| Mission type | Venus orbiter/lander |
| Operator | Roscosmos |
| Mission duration | Orbiter: ≥3 years[1] Lander: >3 hours[2] LLISSE surface probe: ≈90 Earth days[2] |
| Spacecraft properties | |
| Manufacturer | NPO Lavochkin |
| Launch mass | 4,800 kg (10,600 lb)[3] |
| Dry mass | Orbiter: 990 kg (2,180 lb)[4] Lander: 1,600 kg (3,500 lb)[5] |
| Payload mass | Orbiter: 1,200 kg (2,600 lb)[4] Lander: 85 kg (187 lb)[3] |
| Power | Orbiter: 1,700 W [4] |
| Start of mission | |
| Launch date | Proposed: 2031[3] |
| Rocket | Angara A5[4] |
| Launch site | Vostochniy Site 1A[6] |
| Orbital parameters | |
| Reference system | Cytherocentric |
| Regime | Polar |
| Pericytherion altitude | 300 km (190 mi) |
| Apocytherion altitude | 500 km (310 mi)[4] |
| Inclination | 90° |
| Period | 24 hours[4][2] |
| Venus orbiter | |
| Spacecraft component | Orbiter |
| Venus lander | |
| Spacecraft component | Lander |
| Venus Aerial | |
| Spacecraft component | Balloon |
| Transponders | |
| Band | X band, Ka band[4] |
| Capacity | 16 Mbit/sec[4] |
Venera-D will be the first Venus probe launched by the Russian Federation (the earlier Venera probes were launched by the former Soviet Union). Venera-D will serve as the flagship for a new generation of Russian-built Venus probes, culminating with a lander capable of withstanding the harsh Venusian environment for more than the 11⁄2 hours logged by the Soviet probes. The surface of Venus experiences average temperatures of 462 °C (864 °F), crushing 90 bar (89 atm; 1,300 psi) pressures, and corroding clouds of carbon dioxide laced with sulfuric acid. Venera-D will be launched on an Angara A5 rocket.[4]
History
editIn 2003, Venera-D was proposed to the Russian Academy of Sciences for its "wish list" of science projects to be included into the Federal Space Program in 2006–2015. During the formulation of the mission concept in 2004, the launch of Venera-D was expected in 2013 and its landing on the surface of Venus in 2014.[8] In its original conception, it had a large orbiter, a sub-satellite, two balloons, two small landers, and a large long-lived lander (≈3 h).
By 2011, the mission had been pushed back to 2018, and scaled back to an orbiter with a subsatellite orbiter, and a single lander with an expected 3-hour operation time.[9] By the beginning of 2011, the Venera-D project entered Phase A (Preliminary Design) stage of development.
Following the loss of the Phobos-Grunt spacecraft in November 2011 and resulting delays in all Russian planetary projects (with the exception of ExoMars, a joint effort with the European Space Agency), the implementation of the project was again delayed to no earlier than 2026.[7][10]
The possible detection of phosphine in Venus's atmosphere by ALMA in September 2020 spurred a renewed push to implement the Venera-D project. As of 2023, Venera-D is planned for launch no earlier than 2031.[3]
Status
editLavochkin Association are leading the effort in the development of the mission concept architecture. From 2018 to 2020, the second phase of the science activities between NASA and the Russian Space Research Institute (IKI) continued to refine the science concepts, the orbiter and lander mission architecture, as well as a detailed examination of the types of aerial platforms that could address key Venus science in situ.[11][12] Additional workshops were held as the mission concept develops.[11][12][13] From the standpoint of total mass delivered to Venus, the best launch opportunities occur in 2029 and 2031.[14][11]
Goals
editThe mission has an emphasis on the atmospheric superrotation, the geological processes that have formed and modified the surface, the mineralogical and elemental composition of surface materials, and the chemical processes related to the interaction of the surface and the atmosphere.[10]
- Study of the dynamics and nature of superrotation, radiative balance, and the nature of the greenhouse effect
- Characterize the thermal structure of the atmosphere, winds, thermal tides, and solar locked structures
- Measure the composition of the atmosphere, study the clouds, their structure, composition, microphysics, and chemistry
- Investigate the upper atmosphere, ionosphere, electrical activity, magnetosphere, and the gas escape rate
- Perform chemical analysis of surface materials and study the elemental composition of the surface, including radiogenic elements
- Study of interaction between the surface and the atmosphere
- Investigate the structure and chemical composition of the atmosphere down to the surface, including the abundances and isotopic ratios of the trace and noble gases
- Perform direct chemical analysis of the cloud aerosols
- Characterize the geology of local landforms at different scales
Notional science instruments
editTo achieve the mission's science goals, the team is assessing the following instruments for the orbiter:[5]
- PFS-VD Fourier transform spectrometer, 250–2000 cm-1 λ=5-45 μm, Δν = 1 cm-1
- UV mapping spectrometer, 190–490 nm, Δʎ=0.3 nm
- MM-radiometer, Millimeter Wave Radiometer; Ka, V and W bands
- UV-IR Imaging Spectrometer, VENIS
- Monitoring camera
- Solar and star occultation spectrometer, SSOE
- Infrared heterodyne spectrometer, IVOLGA
- Radio-science 1 Orbiter to ground, two-frequency occultation in S- and X-bands
- Radio-science 2 Ground to orbiter two-frequency occultation in S- and X-bands
- GROZA-SAS2-DFM-D, Electromagnetic waves generated by lightning and other electric phenomena
- Suite of 3 plasma instruments: 1) Panoramic energy mass-analyzer of ions; 2) CAMERA-O, electron spectrometer ELSPEC, fast neutrals analyzer FNA; 3) Energetic particle spectrometer.
- Lander instruments
The lander will carry about 85 kg of instruments,[3] that may include:[5]
- Mossbauer Spectrometer / APXS
- Chemical analyses package (CAP): Gas Chromatograph & Mass Spectrometer
- Meteorological suite
- Sample acquisition, handling, processing
Potential NASA collaboration
editIn 2014, Russian scientists asked NASA if the U.S. space agency would be interested in collaborating some instruments to the mission.[7][1] Under this potential collaboration, the study team "Venera-D Joint Science Definition Team" (JSDT) was established in 2015. Venera-D could incorporate some US components, including balloons, a subsatellite for plasma measurements, or a long-lived (90-day) surface station on the lander.[2][10] Any potential collaboration is still under discussion.[1][2][15]
Potential science instruments NASA could contribute include a Raman spectrometer and an Alpha-Proton X-Ray Spectrometer (APXS).[16] Also, the three types of atmospheric maneuverable platforms under consideration by NASA include super pressure balloons, altitude controlled balloons, the Venus Atmospheric Maneuverable Platform (VAMP) semi-buoyant aircraft, and solar powered aircraft.[11][17]
The solar-powered Venus Atmosphere Mobile Platform (VAMP) is currently under development by the Northrop-Grumman Corp. If included, it would be capable of flying within the cloud layer between 50 and 62 km, and is being developed to operate over the 117 Earth days needed for complete monitoring over one full Venus day.[5] It would carry instruments to acquire observations of the atmospheric structure, circulation, radiation, composition and trace gas species, along with cloud aerosols and the unknown ultraviolet absorber(s).[5]
Another proposed payload is LLISSE (Long Lived In-situ Solar System Explorer), which uses new materials and heat-resistant electronics that would enable independent operation for about 90 Earth days.[2][15] This endurance may allow to obtain periodic measurements of weather data to update global circulation models and quantify near surface atmospheric chemistry variability.[2] Its anticipated instruments include wind speed/direction sensors, temperature sensors, pressure sensors, and a chemical multi-sensor array. LLISSE is a small 20 cm (7.9 in) cube of about 10 kg (22 lb).[2][18] The lander may carry two LLISSE units; one would be battery-powered (3,000 h), and the other would be wind-powered.[2][15]
As a result of US sanctions imposed as a result of the 2022 Russian invasion of Ukraine, Roscosmos Director-General Dmitry Rogozin announced that any continued participation between Russia and the United States on Venera-D was inappropriate.[19]
See also
editReferences
edit- ^ a b c "NASA Studying Shared Venus Science Objectives with Russian Space Research Institute". NASA. 10 March 2017. Retrieved 2 January 2023.
- ^ a b c d e f g h i j Venera-D: Phase II Final Report. Joint Science Definition Team. 31 January 2019.
- ^ a b c d e f Zak, Anatoly (5 March 2021). "New promise for the Venera-D project". RussianSpaceWeb. Retrieved 7 March 2021.
- ^ a b c d e f g h i Status Report of the Venera-D Joint Science Definition Team. D. Senske, L. Zasova, A. Burdanov, T. Economou, N. Eismont, M. Gerasimov, D. Gorinov, J. Hall, N. Ignatiev, M. Ivanov, K. Lea Jessup, I. Khatuntsev, O. Korablev, T. Kremic, S. Limaye, I. Lomakin, A. Martynov, A. Ocampo, S. Teselkin, O. Vaisberg, and V. Vorontsov. Lunar and Planetary Institute conference. 11 December 2017.
- ^ a b c d e Venera-D: Expanding our horizon of terrestrial planet climate and geology through the comprehensive exploration of Venus. Report of the Venera-D Joint Science Definition Team. 31 January 2017.
- ^ Venera-D Mission Concept for Study Atmosphere, Surface and Plasma Environment of Venus. 42nd COSPAR Scientific Assembly. Held 14–22 July 2018, in Pasadena, California, USA, Abstract id. PEX.1-26-18. July 2018.
- ^ a b c d e Wall, Mike (17 January 2017). "Russia, US Mulling Joint Mission to Venus". Space. Retrieved 29 October 2017.
- ^ Venera-D mission at Russia Space Web (accessed 25 November 2013)
- ^ Ted Stryk, Russia's Venera-D mission (DPS-EPSC 2011), Planetary Society, 10 May 2011 (accessed 25 November 2013)
- ^ a b c Senske, D.; Zasova, L. (31 January 2017). "Venera-D: Expanding our horizon of terrestrial planet climate and geology through the comprehensive exploration of Venus" (PDF). NASA. Archived from the original (PDF) on 27 April 2017. Retrieved 29 October 2017.
- ^ a b c d e f Development of the Venera-D Mission Concept, from Science Objectives to Mission architecture. 49th Lunar and Planetary Science Conference 2018 (LPI Contrib. No. 2083).
- ^ a b Venera-D Phase II. LPI. 2019.
- ^ An Airship for Exploring Venus? Russia Might Get There First. Dirk Schulze-Makuch, Air & Space Magazine. 11 October 2019.
- ^ "РАН назвала сроки запуска и стоимость «Венеры-Д»".
- ^ a b c Long Lived In-situ Solar System Explorer (LLISSE). LPI. 2019.
- ^ Report of the Venera-D Joint Science Definition Team. 31 January 2017. JSDT, VEXAG at NASA.
- ^ Solar Airplane Concept Developed for Venus Exploration. (PDF) NASA. Glenn Research Center. 2018.
- ^ NASA's space probe for exploring Venus should be ready by 2023. Alison DeNisco Rayome, C-Net. 23 October 2019.
- ^ @katlinegrey (26 February 2022). "Roscosmos won't cooperate with USA in working on #VeneraD mission, said Rogozin. In my personal opinion, only this…" (Tweet) – via Twitter.
External links
edit- Venera-D – Federal Space program of Russian Federation Archived 31 July 2017 at the Wayback Machine
- Venera-D mission at Russia Space Web
- Venera-D Phase II Report (31 January 2019)