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imagery related to the subject. Please contact <a href="mailto:(Anatoly Zak) agzak@russianspaceweb.com">Anatoly Zak</a>.</p> <hr align="left"> <p align="center" class="tableText">The author would like to thank the director of Moscow's Space Research Institute, Lev Zeleny and his colleagues at IKI Oleg Korablev and Ludmila Zasova, as well as Hakan Svedhem, Franco Bonacina, Amruta Mehta at ESA and Francis Rocard at CNES for their tremendous help in preparing this section.</p> </td> <td align="left" valign="top" bordercolor="#CCCCCC" bgcolor="#FFFFFF" ><p align="center" class="mainHeadline">Venera-D to return to Venus in the 21st century</p> <p class="quickDesc">Venera-D, where "D" stands for Dolgozhivushaya (long-lasting), became the first Russian project in the post-Soviet period aimed to explore Venus. Also, it was to be the second Russian planetary mission heading beyond lunar orbit after the <a href="phobos_grunt.html">Phobos-Grunt</a> project. Venera-D promised to expand human knowledge about history of the Earth's closest neighbor in the Solar System, particularly about the fate of ancient water on its surface.</p> <p align="left" class="navLine"><font face="Verdana, Arial, Helvetica, sans-serif">Previous chapter: <a href="phobos_grunt2.html">Phobos-Grunt-2 mission</a></font></p> <hr> <p> </p> <p align="center"><img src="images/spacecraft/planetary/venus/venera_d/venera_d_var2_2009_1.jpg" alt="Venera-D Variant 2" width="600" height="408"></p> <p align="left" class="picCaption">The Venera-D spacecraft approaching clouds-veiled Venus. Shown configuration was only one of several designs envisioned at the conclusion of the project's definition phase in September 2009. A ball-shaped capsule containing the main lander can be seen at the top, with four mini-capsules carrying atmospheric balloons attached just below it. Individual entry capsules for each balloon would allow to deploy scientific sensors over much wider regions of the planet then it would be possible if they were all released from a single descent vehicle.</p> <hr> <p class="subheadLine">Origin of the Venera-D project</p> <p class="bodyText">In 2003, Russian Academy of Sciences was drafting its "wish list" of scientific projects to be included into the Federal Space Program in 2006-2015. After more than a decade-long slump, Russian space scientists at the Academy's Space Research Institute, IKI, could look forward for new projects. For the Federal Program, Vasily Moroz, one of the leading scientists at IKI, and a veteran of several <a href="spacecraft_planetary_venus.html">Soviet missions to Venus</a> and <a href="spacecraft_planetary_mars.html">Mars</a>, proposed a new mission to the Earth's closest neighbor in the Solar System. The project dubbed Venera-D would build up on completed missions, as well as on unfulfilled projects in the former USSR. The highlight of the future mission would be a longer survival of the lander on the stove-hot surface of Venus, comparing to an roughly hour-long lifespan of previous Soviet spacecraft.</p> <p class="subheadLine">How long is the long duration?</p> <p class="bodyText">During the formulation of the mission concept in <a href="chronology_2004.html">2004</a>, the launch of the Venera-D spacecraft was expected in <a href="2013.html">2013</a> and its landing on the surface of Venus in <a href="2014.html">2014</a>. As the extended survival on the surface of Venus seemed to be the main goal of the mission at the time, planners had first to decide to what length of stay they could shoot for. This single property would mainly determine the technical challenges to the project and the overall cost of the mission. On May 19, 2005, the Space Council of the Academy of Sciences held a meeting discussing a proposal of the Academy for the Federal Space Program. A special Addition No. 2 to the transcript of the meeting defined long duration as 30 days.</p> <p class="bodyText">On October 22, 2005, the Russian government signed a decree No. 635, approving Federal Space Program for 2006-2015. It included funding for the Venera-D project, envisioning a long-duration lander on the surface of Venus, which could function 30 days. Speaking at the 5th International Aerospace Congress in Moscow, on August 29, <a href="2006.html">2006</a>, Deputy Chief of the Federal Space Agency, Vitaly Davydov, listed Venera-D among high-priority exploration projects funded by the Russian government. However level and timing of funding projected by the government would not enable the launch of the mission before 2016. Estimates during 2007 quoted a 2016-2018 launch window, which was contingent on the immediate beginning of funding. During 2007-2009, available money afforded a definition study only, with full-scale development anticipated in <a href="2010.html">2010</a>.</p> <p class="bodyText">During <a href="2006.html">2006</a> and <a href="2007.html">2007</a>, Russian and European representatives discussed the possibility of a cooperative mission, which could include a European orbital module, an atmospheric balloon, small landing probes, a Russian lander and a Japanese atmospheric balloon. A total of three or four balloons could be dropped into the atmosphere, where they could function for more than a day at altitudes from 60 to 10 kilometers and some could even land and survive on the boiling surface of Venus for more than an hour. (<a href="sources.html#sanko">364</a>)</p> <p class="bodyText">At the time, the spacecraft was expected to be launched by the <a href="soyuz2_lv.html">Soyuz-2 rocket</a> with the <a href="fregat.html">Fregat upper stage</a> from an <a href="kourou_els.html">equatorial facility</a> in <a href="kourou.html">Kourou</a>, French Guiana.</p> <p class="tableHeadline">Mass specifications of the Venera-D spacecraft, as of Jan. 24, 2007 (<a href="sources.html#sanko">364</a>):</p> <table width="100%" border="0" cellspacing="0" cellpadding="3"> <tr> <td bgcolor="#CCCCCC" class="tableText">Low-Earth parking orbit*</td> <td bgcolor="#CCCCCC" class="tableText">8,120 kilograms</td> </tr> <tr> <td class="tableText">Near Venus</td> <td class="tableText">1,900 kilograms</td> </tr> <tr> <td bgcolor="#CCCCCC" class="tableText">Descent probe</td> <td bgcolor="#CCCCCC" class="tableText">1,100 kilograms</td> </tr> <tr> <td class="tableText">A three-day orbit (orbiter)</td> <td class="tableText">600 kilograms</td> </tr> </table> <hr> <p class="footerCredit">*including an Earth-orbit escape stage based on the <a href="regat.html">Fregat</a> orbital tug;</p> <hr> <p class="bodyText">During <a href="2008.html">2008</a>, Space Research Institute, IKI, issued a report summarizing the results of the second and final stage in the research and development study, NIR, entitled "Development of methods for complex research of Venus with the use of an orbiter, balloons, and a long-duration lander," also known as Venera-GLOB. The document formulated scientific tasks of the Venera-D mission and determined composition and characteristics of scientific instruments for an orbiter, atmospheric probes and a lander. IKI argued that simultaneous, long-duration observations from the surface, orbit and in the atmosphere could bring exploration of Venus to a radically new level.</p> <p class="bodyText">After the selection of scientific instruments, IKI recommended following payload characteristics:</p> <ul> <li class="bodyText">Orbiter: 40-50 kilograms;</li> <li class="bodyText">Atmospheric balloon: no less than 20 kilograms and a lifespan of no less than five days;</li> <li class="bodyText">Lander: 10-15 kilograms, including a small long-duration module with around 4.5 kilograms of scientific gear for a high-risk part of the mission;</li> </ul> <p class="bodyText">The same IKI effort also evaluated a possible Russian contribution into the proposed European mission to Venus, known as EVE. It envisioned a 170-kilogram lander delivering 25 kilograms of scientific gear onto the surface of Venus. However by <a href="2009.html">2009</a>, ESA did not expect the EVE mission to fly until around 2024.</p> <p class="subheadLine">Venus scientists of the world, unite!</p> <p class="bodyText">IKI scientists invited a wide cooperation on the Venera-D project. The first of what hoped to be an annual international conference, dedicated to the Venera-D prpject was held at IKI on Sept. 30 - Oct. 2, 2009. By that time, Russian planners apparently felt confident enough in the future funding and in support from abroad to draft additional heavier versions of the Venera-D mission, based on the use of more powerful and expensive launch vehicles than <a href="soyuz2_lv.html">Soyuz-2</a>:</p> <table width="100%" border="0" cellspacing="0" cellpadding="3"> <tr> <td valign="bottom" bgcolor="#CCCCCC" class="tableText">-</td> <td valign="bottom" bgcolor="#CCCCCC" class="tableHeader"><div align="right">Variant 1</div></td> <td valign="bottom" bgcolor="#CCCCCC" class="tableHeader"><div align="right">Variant 1</div></td> <td valign="bottom" bgcolor="#CCCCCC" class="tableHeader"><div align="right">Variant 3</div></td> </tr> <tr> <td bgcolor="#FFFFFF" class="tableText">Launch vehicle</td> <td bgcolor="#FFFFFF" class="tableText"><div align="right"><a href="soyuz2_lv.html">Soyuz-2-1b</a></div></td> <td bgcolor="#FFFFFF" class="tableText"><div align="right" class="bodyText"> <div align="right"><a href="zenith.html" class="tableText">Zenit</a></div> </div></td> <td bgcolor="#FFFFFF" class="tableText"><div align="right" class="tableText"> <div align="right">***<a href="proton.html">Proton</a></div> </div></td> </tr> <tr> <td bgcolor="#CCCCCC" class="tableText">Spacecraft mass in the low-Earth orbit</td> <td bgcolor="#CCCCCC" class="tableText"><div align="right">7,750 kg</div></td> <td bgcolor="#CCCCCC" class="tableText"><div align="right">12,000 kg</div></td> <td bgcolor="#CCCCCC" class="tableText"><div align="right">20,000 kg</div></td> </tr> <tr> <td bgcolor="#FFFFFF" class="tableText">Propellant mass for reaching Earth-escape velocity</td> <td bgcolor="#FFFFFF" class="tableText"><div align="right">5,350 kg</div></td> <td bgcolor="#FFFFFF" class="tableText"><div align="right">8,035 kg</div></td> <td bgcolor="#FFFFFF" class="tableText"><div align="right">13,600 kg</div></td> </tr> <tr> <td bgcolor="#CCCCCC" class="tableText">Propulsion module dry mass</td> <td bgcolor="#CCCCCC" class="tableText"><div align="right">1,050 kg</div></td> <td bgcolor="#CCCCCC" class="tableText"><div align="right">1,500 kg</div></td> <td bgcolor="#CCCCCC" class="tableText"><div align="right">2,700 kg</div></td> </tr> <tr> <td bgcolor="#FFFFFF" class="tableText">Propellant mass for orbit correction</td> <td bgcolor="#FFFFFF" class="tableText"><div align="right">45 kg</div></td> <td bgcolor="#FFFFFF" class="tableText"><div align="right">65 kg</div></td> <td bgcolor="#FFFFFF" class="tableText"><div align="right">110 kg</div></td> </tr> <tr> <td bgcolor="#CCCCCC" class="tableText">Propellant mass for Venus orbit insertion</td> <td bgcolor="#CCCCCC" class="tableText"><div align="right">345 kg</div></td> <td bgcolor="#CCCCCC" class="tableText"><div align="right">460 kg</div></td> <td bgcolor="#CCCCCC" class="tableText"><div align="right">1,000 kg</div></td> </tr> <tr> <td bgcolor="#FFFFFF" class="tableText">Spacecraft mass in the orbit of Venus</td> <td bgcolor="#FFFFFF" class="tableText"><div align="right">1,080 kg</div></td> <td bgcolor="#FFFFFF" class="tableText"><div align="right">*1,540 kg</div></td> <td bgcolor="#FFFFFF" class="tableText"><div align="right">**2,200 kg</div></td> </tr> </table> <hr> <p class="footerCredit">*1,340 kg, according to previous data; **3,500 kg according to previous data; ***The <a href="angara.html">Angara rocket</a> was apparently also under consideration for Variant 3 launch, as an alternative to Proton;</p> <hr> <p class="subheadLine">Mission description</p> <p class="bodyText">By 2009, a "base" Venera-D mission, which would be launched by the Soyuz-2-1b rocket included following components:</p> <table width="100%" border="0" cellspacing="0" cellpadding="3"> <tr> <td width="10%" valign="bottom" bgcolor="#CCCCCC" class="tableHeader">Element</td> <td width="10%" valign="bottom" bgcolor="#CCCCCC" class="tableHeader"><div align="right">Mass</div></td> <td width="11%" valign="bottom" bgcolor="#CCCCCC" class="tableHeader"><div align="right">Payload mass</div></td> <td width="69%" valign="bottom" bgcolor="#CCCCCC" class="tableHeader">Mission details</td> </tr> <tr> <td bgcolor="#FFFFFF" class="tableText">Orbiter</td> <td bgcolor="#FFFFFF" class="tableText"><div align="right">600 kg</div></td> <td bgcolor="#FFFFFF" class="tableText"><div align="right">50.0 kg</div></td> <td bgcolor="#FFFFFF" class="tableText">A two-year (six Venus days) lifespan with 50-60 kilograms of payload; (<a href="sources.html#sanko">364</a>)</td> </tr> <tr> <td bgcolor="#CCCCCC" class="tableText">Balloon No. 1</td> <td bgcolor="#CCCCCC" class="tableText"><div align="right">150 kg</div></td> <td bgcolor="#CCCCCC" class="tableText"><div align="right">5.0 kg</div></td> <td bgcolor="#CCCCCC" class="tableText">A 3.4-meter in diameter balloon inherited from Vega mission; High-atmosphere, 55-60 kilometers altitude with an eight-day lifespan;</td> </tr> <tr> <td bgcolor="#FFFFFF" class="tableText">Balloon No. 2</td> <td bgcolor="#FFFFFF" class="tableText"><div align="right">150 kg</div></td> <td bgcolor="#FFFFFF" class="tableText"><div align="right">15.0 kg</div></td> <td bgcolor="#FFFFFF" class="tableText">Below-clouds, 45-50 kilometers altitude with an eight-day lifespan; could carry "microprobes" as a ballast to be dropped on the surface;</td> </tr> <tr> <td bgcolor="#CCCCCC" class="tableText">Micro-probes</td> <td bgcolor="#CCCCCC" class="tableText"><div align="right">2 kg</div></td> <td bgcolor="#CCCCCC" class="tableText"><div align="right">0.2 kg</div></td> <td bgcolor="#CCCCCC" class="tableText">Up to four 0.2-meter in diameter microprobes could be dropped from balloons one after another;</td> </tr> <tr> <td bgcolor="#FFFFFF" class="tableText">Lander</td> <td bgcolor="#FFFFFF" class="tableText"><div align="right">150-170 kg</div></td> <td bgcolor="#FFFFFF" class="tableText"><div align="right">20.0-25.0 kg</div></td> <td bgcolor="#FFFFFF" class="tableText">Designed for 1.5-hour descent and one-hour lifespan after touchdown in Tesserae area of Venus;</td> </tr> </table> <hr> <p class="subheadLine">The orbiter</p> <p class="bodyText">As in a typical planetary mission, the orbiting component of the Venera-D mission would be used to relay data back to Earth from scientific payloads in the atmosphere and on the surface of Venus. The orbiter's main science goals would be research into the composition of the planet's atmosphere and its circulation patterns.</p> <p class="subheadLine">Balloons</p> <p class="bodyText">A pair of balloons would be dropped from the lander during its descent at two different altitudes. They would measure acoustic and electrical activities in the Venusian skies for up to eight days.</p> <p class="subheadLine">Microprobes</p> <p class="bodyText">Up to four microprobes could dropped from balloons. During their approximately 30-minute descent, they would continuously probe the atmosphere in multiple locations.</p> <p class="subheadLine">The lander</p> <p class="bodyText">A lander was designed for studies of the atmospheric composition and clouds during its descent and analyze soil after its touchdown. As of 2009, experiments with soil would not involve bringing of samples onboard the lander. (<a href="sources.html#korablev">365</a>) Also, original plans to keep the lander operating for a month were dropped due to many technological challenges of building heat-resistant electronics and their high price tag.</p> <p class="subheadLine">Cruise stage</p> <p class="bodyText">As of 2009, Venera-D mission was expected to use a standardized cruise stage originally developed for the <a href="phobos_grunt.html">Phobos-Grunt project</a>. The vehicle would take over all maneuvering functions of the mission after the Fregat upper stage sends Venera-D from the low-Earth parking orbit to the escape trajectory to Venus and separates. The cruise stage would use its own propulsion system for the trajectory corrections during the journey between the Earth and Venus, as well as for braking maneuver to enter the orbit around Venus.</p> <p class="subheadLine">Wind flyer</p> <p class="bodyText">In addition, to "classical" means of exploring Venus, which were all tried during the Soviet period, NPO Lavochkin proposed an innovative "vetrolet" (a Russian term for "wind flyer") for the Venera-D project. A kite-like device would take advantage of winds in the atmosphere of Venus, which reportedly would allow it to glide at the altitude of 45-50 kilometers almost indefinitely, or at least a month in a realistic mission scenario. </p> <p class="bodyText">An innovative vehicle could probably join the mission only as a concept demonstrator rather than a full-fledged platform for scientific instruments. An additional mass associated with the device would likely require a switch from the Soyuz to Zenit as a carrier of the Venera-D mission. The information about the Vetrolet first surfaced in August 2009 and NPO Lavochkin apparently made a presentation about the vehicle at the Venera-D conference in IKI a month later. By that time, some prototypes of the flyer had already been tested, Lavochkin's sources said.</p> <hr> <p class="bodyText"><strong><a name="cd"></a></strong><span class="subheadLine">Chief-designers council</span></p> <p class="bodyText">On Nov. 24, 2009, key officials in the Venera-D project, including experts from TsNIIMash research institute, IKI, and MAI, held a meeting at NPO Lavochkin, discussing technical report entitled "The formation of the preliminary design of the spacecraft for long-duration exploration of Venus." V. A. Vorontsov, the chief designer of Venera-D, presented a master schedule for the project. According to NPO Lavochkin's press-release, at the time, the organization's experience in the development of <a href="spacecraft_planetary_venus.html">Venera</a>, Vega and <a href="phobos_grunt.html">Phobos-Grunt spacecraft</a> was studied for possible application in the Venera-D project.</p> <p class="bodyText">The outcome of the chief-designer council meeting was the decision to evaluate the use of <a href="proton.html">Proton</a> and <a href="angara.html">Angara</a> launch vehicles for the mission. The participants also had to consider the construction of a high-pressure test chamber (mimicking conditions on Venus) or find adequate existing facilities. A test chamber, which was previously used for testing Vega spacecraft, apparently fell in disrepair.</p> <p class="subheadLine">Chinese involvement</p> <p class="bodyText">In 2010, at an aerospace exhibit in China, representatives of the Russian space agency said that they discussed possible Russian-Chinese cooperation on a mission to Venus.</p> <p class="bodyText"><a name="2011"></a><span class="subheadLine">Develeopments during 2011 and 2012</span></p> <p class="bodyText">By the beginning of 2011, the Venera-D project entered Phase A (Preliminary Design) stage of development. By that time, the composition of the project had changed to include a lander, a main orbiter and an additional small satellite of Venus dedicated to studies of plasma environment around the planet. Previous plans to release balloons in the Venusian atmosphere had to be abandoned, as apparently were additional landers and an atmospheric flyer. An option to fly these technically challenging and likely expensive original components of the Venera-D project were deferred to a follow-on Venera missions, possibly a <a href="spacecraft_planetary_venus.html#vg">Venera-Glob</a> project with a proposed launch date in 2021. The composition of scientific instruments onboard Venera-D also <a href="#2011payloads">changed</a>. </p> <p class="bodyText">A sub-satellite was proposed for simultaneous measurements with plasma instruments onboard the main orbiter. The orbiter was to be inserted into a polar orbit, which would take a full day to complete. The landing site was preliminary chosen at one of the so-called tesseras -- the oldest areas, where non-basaltic material could be found, which had formed before the period of high volcanic activity around 700 million years ago. (<a href="sources.html#zasova2">514</a>)</p> <p class="bodyText">In the meantime, Venera-D itself faced a tough competition for the timeframe of its launch, as well as for available funding in the <a href="russia_2010s.html">Russian space program during 2010s</a>, particularly with the <a href="marsnet.html">Mars-NET project</a>, which was expected to head to Mars, following <a href="phobos_grunt.html">Phobos-Grunt</a> mission in <a href="2011.html">2011</a>, <a href="luna_resurs.html">Luna-Resurs</a> in <a href="2013.html">2013</a> and <a href="luna_glob.html">Luna-Glob</a> in <a href="2014.html">2014</a>, respectively. Proposals for similar missions to Venera-D in Europe and US, which could provide a basis for cooperation with Russia, all lost competition for funding in the selection process at NASA and ESA and, as a result, had to be deferred to <a href="chronology_XXI.html">2020s</a>. (<a href="sources.html#zeleny2">513</a>) Still, the official launch date of Venera-D was then expected in <a href="2017.html">2017</a>, just one year behind a previous timeline and, apparently, a year after the projected <a href="2016.html">launch</a> of <a href="marsnet.html">Mars-NET</a>.</p> <p class="bodyText">However following the <a href="phobos_grunt_launch.html">loss</a> of <a href="phobos_grunt.html">Phobos-Grunt</a> spacecraft in November 2011 and resulting delays in all Russian planetary projects, the Venera-D quickly lost priority. In April 2012, one strategy document quoted by the official <em>RIA Novosti</em> news agency pushed the implementation of the project to no earlier than 2024. The authors of the document argued that even such remote launch dates would be possible only on the condition that Russia would start immediate revival of necessary testing infrastructure and technological capabilities. In the meantime, a proposal for the follow-on Venera-Glob mission had to be deferred indefinitely.</p> <p class="bodyText">In August 2012, a presentation by NPO Lavochkin placed the Venera-D mission to 2026, at the very back of a long line of planned spacecraft and even behind the project to bring back soil samples from Mars!</p> <p class="subheadLine">Venera-D project timeline (as of 2009):</p> <p class="bodyText"><strong>2007-2010 January: </strong>A mission definition phase (NIR). (<a href="sources.html#korablev">365</a>)</p> <p class="bodyText"><strong>2010-2011:</strong> A/B development stage (NIOKR). (<a href="sources.html#korablev">365</a>)</p> <p class="bodyText"><strong>2012-2016:</strong> C/D development stage (OKR). (<a href="sources.html#korablev">365</a>)</p> <p class="bodyText"><strong>2016 Dec. 6:</strong> The launch of the Venera-D spacecraft toward Venus.</p> <p class="bodyText"><strong>2017 May 16:</strong> Venera-D arrives to Venus.</p> <p class="bodyText"><strong>2019:</strong> End of mission. (<a href="sources.html#korablev">365</a>)</p> <hr> <p class="tableHeadline"> </p> <p class="tableHeadline">Masses of proposed payloads onboard Venera-D, as of Jan. 24, 2007 (<a href="sources.html#sanko">364</a>):</p> <table width="100%" border="0" cellspacing="0" cellpadding="3"> <tr> <td colspan="2" bgcolor="#000000" class="tableHeader style1">Orbiter </td> </tr> <tr> <td class="tableText">Fourier spectrometer for 0,9–50 mm</td> <td class="tableText">25.0 kg</td> </tr> <tr> <td bgcolor="#CCCCCC" class="tableText">Imaging UV-spectrometer 0,19–0,49 mm</td> <td bgcolor="#CCCCCC" class="tableText">5.0 kg</td> </tr> <tr> <td class="tableText">Wide-angle CCD camera with several channels 0,23–1,02 mm</td> <td class="tableText">0.5 kg</td> </tr> <tr> <td bgcolor="#CCCCCC" class="tableText">High resolution limb spectrometer</td> <td bgcolor="#CCCCCC" class="tableText">5.0 kg</td> </tr> <tr> <td class="tableText">Radiometer</td> <td class="tableText">1.0 kg</td> </tr> <tr> <td bgcolor="#CCCCCC" class="tableText">Radio science</td> <td bgcolor="#CCCCCC" class="tableText">1.0 kg</td> </tr> <tr> <td class="tableText">Plasma complex (including ion mass spectrometer)</td> <td class="tableText">2.0 kg</td> </tr> <tr> <td colspan="2" bgcolor="#000000" class="tableHeader style1">Balloons </td> </tr> <tr> <td class="tableText">Meteo-complex</td> <td class="tableText">0.3 kg</td> </tr> <tr> <td bgcolor="#CCCCCC" class="tableText">Mini fourier spectrometer</td> <td bgcolor="#CCCCCC" class="tableText">1.5 kg</td> </tr> <tr> <td class="tableText">CCD camera</td> <td class="tableText">0.5 kg</td> </tr> <tr> <td bgcolor="#CCCCCC" class="tableText">Nepfelometer</td> <td bgcolor="#CCCCCC" class="tableText">0.5 kg</td> </tr> <tr> <td class="tableText">Radiometer</td> <td class="tableText">0.5 kg</td> </tr> <tr> <td colspan="2" bgcolor="#000000" class="tableText"><span class="tableHeader style1">Lander </span> <div align="right"></div></td> </tr> <tr> <td class="tableText">Neutral mass spectrometer</td> <td class="tableText">6.0 kg</td> </tr> <tr> <td bgcolor="#CCCCCC" class="tableText">Experiment for surface properties investigations</td> <td bgcolor="#CCCCCC" class="tableText">3.0 kg</td> </tr> <tr> <td class="tableText">Meteocomplex</td> <td class="tableText">0.3 kg</td> </tr> <tr> <td bgcolor="#CCCCCC" class="tableText">Mini fourier spectrometer</td> <td bgcolor="#CCCCCC" class="tableText">1.5 kg</td> </tr> <tr> <td class="tableText">CCD camera</td> <td class="tableText">0.5 kg</td> </tr> <tr> <td bgcolor="#CCCCCC" class="tableText">Seismometer</td> <td bgcolor="#CCCCCC" class="tableText">3.0 kg</td> </tr> <tr> <td class="tableText">Nephelometer</td> <td class="tableText">0.5 kg</td> </tr> <tr> <td bgcolor="#CCCCCC" class="tableText">Radiometer</td> <td bgcolor="#CCCCCC" class="tableText">0.5 kg</td> </tr> </table> <p class="bodyText">Scientific goals of the Venera-D mission, as of Jan. 24, 2007 (<a href="sources.html#sanko">364</a>):</p> <p class="subheadLine">Orbiter</p> <ul> <li class="bodyText">The 3D temperature and wind field in the middle atmosphere, its local time and temporal variations. Investigations of the thermal tides;</li> <li class="bodyText">Nature, composition and optical properties of the clouds;</li> <li class="bodyText">Nature of “unknown”UV absorber;</li> <li class="bodyText">Dynamics and nature of superrotation</li> <li class="bodyText">Chemical composition of the atmosphere: H2O, SO2, CO, HCl, HF etc.;</li> <li class="bodyText">Surface temperature, volcanic activity, lightning;</li> <li class="bodyText">Plasma environment.</li> </ul> <p class="subheadLine">Balloons</p> <ul> <li class="bodyText">Dynamics of the atmosphere;</li> <li class="bodyText">Meteorology (pressure, temperature density with high accuracy);</li> <li class="bodyText">Chemical composition and optical properties of the clouds;</li> <li class="bodyText">Chemical composition of the atmosphere;</li> <li class="bodyText">Imaging of the surface;</li> <li class="bodyText">Radiative balance and greenhouse effect;</li> <li class="bodyText">Surface temperature;</li> <li class="bodyText">Possible volcanic activity, lightning.</li> </ul> <p class="subheadLine">Lander</p> <ul> <li class="bodyText">Chemical composition of the atmosphere below 64 km;</li> <li class="bodyText">Abundance (with high accuracy) of noble gases and isotopic composition;</li> <li class="bodyText">Clouds composition and optical properties;</li> <li class="bodyText">Radiativebalance and greenhouse effect;</li> <li class="bodyText">Surface temperature, mineralogical characteristics;</li> <li class="bodyText">Possible volcanic and seismic activity, lightning.</li> </ul> <hr> <p class="bodyText"><strong><a name="2011payloads"></a></strong>Scientific payloads onboard Venera-D, as of 2011 (<a href="sources.html#zeleny2">513</a>):</p> <p class="subheadLine">Orbiter</p> <ul> <li class="bodyText">several spectrometers in the spectral range from UV to MM;</li> <li class="bodyText">the mapping spectrometers; </li> <li class="bodyText">monitoring camera;</li> <li class="bodyText">the plasma package.</li> </ul> <p class="subheadLine">Lander</p> <ul> <li class="bodyText">GC-MS, PTW (meteo), nephelometer and the particle sizes spectrometer; </li> <li class="bodyText">optical package; </li> <li class="bodyText">active gamma spectrometer; </li> <li class="bodyText">Mossbauer spectrometer, MTDL (Multichannel Tunable Diode Laser Spectrometer); </li> <li class="bodyText">LIPS (Laser-Induced Plasma Spectrometer);</li> <li class="bodyText">TV-complex, containing panoramic, high resolution and descending cameras.</li> </ul> <hr> <p class="bodyText">Venera-D development team, as of 2011 (<a href="sources.html#zeleny2">513</a>):</p> <table width="100%" border="0" cellspacing="0" cellpadding="3"> <tr> <td bgcolor="#CCCCCC" class="tableText">NPO Lavochkin</td> <td bgcolor="#CCCCCC" class="tableText">Prime developer</td> </tr> <tr> <td class="tableText">Space Research Institute, IKI</td> <td class="tableText">Science program</td> </tr> <tr> <td bgcolor="#CCCCCC" class="tableText">Vernadsky Geochemistry and Analytical Chemistry Institute, GEOKhI</td> <td bgcolor="#CCCCCC" class="tableText">Science program</td> </tr> <tr> <td class="tableText">Kotelnikov Radiotechnology and Electronics Institute</td> <td class="tableText">-</td> </tr> <tr> <td bgcolor="#CCCCCC" class="tableText">Keldysh Applied Mathematics Institute</td> <td bgcolor="#CCCCCC" class="tableText">Mission planning</td> </tr> <tr> <td class="tableText">Shmidt Earth Physics Institute</td> <td class="tableText">Science program</td> </tr> </table> <hr> <p class="subheadLine"> </p> <p class="navLine">Next chapter: <a href="venera-d-2021.html">Venera-D mission in 2021</a></p> <p class="bodyText"> </p> <p><strong><font size="1" face="Verdana, Arial, Helvetica, sans-serif"></font></strong></p> <p> </p> <p><a class="addthis_button" href="http://www.addthis.com/bookmark.php?v=250&pub=xa-4a9567347f52c441"><img src="http://s7.addthis.com/static/btn/v2/lg-share-en.gif" width="125" height="16" alt="Bookmark and Share" style="border:0"/></a></p> <hr> <p align="center" class="footerCredit">Written by Anatoly Zak; last update: March 5, 2021 </p> <p align="center" class="footerCredit">All rights reserved.</p></td> <td width="200" align="left" valign="top" bordercolor="#CCCCCC" bgcolor="#CCCCCC" ><p align="center"><a href="insider-content.html"><img src="images/logos/insider_content_200.jpg" alt="insider content" width="200" height="486" border="0"></a></p> <p align="center"> </p> <p align="center"><img src="images/spacecraft/planetary/venus/venera82/venera_13_14_surface_2.jpg" alt="Surface of Venus" width="200" height="150"></p> <p align="left" class="picCaptionSidebar"><font face="Verdana, Arial, Helvetica, sans-serif">Color images of hellish surface of Venus obtained by Soviet Venera-13 and Venera-14 spacecraft exemplified the highest achievements in the exploration of the Earth's closest neighbor in the Solar System in the 20th century. Credit: IKI</font></p> <hr> <p align="center" class="picCaptionSidebar"><img src="images/spacecraft/planetary/venus/venera_d/djvs_2.jpg" alt="DJVS" width="200" height="150"></p> <p align="left" class="picCaptionSidebar"><font face="Verdana, Arial, Helvetica, sans-serif">Venera-D project traced its roots to the Soviet project of a long-duration lander on the surface of Venus. Credit: NPO Lavochkin</font></p> <hr> <p align="center" class="picCaptionSidebar"><img src="images/spacecraft/planetary/venus/venera_d/venera_d_c2003_2.jpg" alt="Venera-D" width="200" height="217"></p> <p align="left" class="picCaptionSidebar"><font face="Verdana, Arial, Helvetica, sans-serif">Venera-D spacecraft, as it was depicted before 2007. Credit: NPO Lavochkin</font></p> <hr> <p align="center" class="picCaptionSidebar"><img src="images/spacecraft/planetary/venus/venera_d/venera_d_c2008_2.jpg" alt="Venera-D" width="150" height="200"></p> <p align="left" class="picCaptionSidebar"><font face="Verdana, Arial, Helvetica, sans-serif">An artist depiction of the Venera-D spacecraft, circa 2008. A design borrowed from the cruise stage of the <a href="phobos_grunt.html">Phobos-Grunt spacecraft</a> is easily recognizable, however smaller solar panels would be used due to proximity to the Sun. Notable is a depiction of the reentry craft, shaped like a descent module of Russia's <a href="ppts.html">next-generation manned spacecraft</a> instead of a traditional ball-shaped capsule used in the <a href="spacecraft_planetary_venus.html">Soviet missions to Venus</a>. Credit: IKI</font></p> <hr> <p align="center" class="picCaptionSidebar"><img src="images/spacecraft/planetary/venus/venera_d/venera_d_var1_2009_2.jpg" alt="Variant 1" width="200" height="167"></p> <p align="left" class="picCaptionSidebar"><font face="Verdana, Arial, Helvetica, sans-serif">Variant 1 of the Venera-D design as of September 2009. Credit: NPO Lavochkin/IKI</font></p> <hr> <p class="picCaptionSidebar"><img src="images/spacecraft/planetary/venus/venera_d/c2011_2.jpg" alt="venera-D" width="200" height="143"></p> <p class="picCaptionSidebar"><font face="Verdana, Arial, Helvetica, sans-serif">Artist rendering of the Venera-D spacecraft circa 2011. Credit: IKI</font></p> <hr> <p align="center" class="picCaptionSidebar"><img src="images/spacecraft/planetary/venus/eve/eve_balloon_art_2.jpg" alt="balloon" width="186" height="137"></p> <p align="center" class="picCaptionSidebar"><img src="images/spacecraft/planetary/venus/eve/eve_art_2.jpg" alt="EVE" width="150" height="200"></p> <p align="left" class="picCaptionSidebar"><font face="Verdana, Arial, Helvetica, sans-serif">Artist depiction of a balloon and a lander (possibly Russian-built) on the surface of Venus, proposed within European Venus Explorer project circa 2007. As of 2009, the mission was not expected to take off until around 2025, however. Credit: ESA</font></p> <hr> <p class="picCaptionSidebar"><img src="images/spacecraft/planetary/venus/venera_d/long_lived_station_2017_2.jpg" alt="station" width="200" height="207"></p> <p class="picCaptionSidebar"><font face="Verdana, Arial, Helvetica, sans-serif">A concept of a long-duration station proposed for the Venera-D mission circa 2016. Credit: NASA</font></p> <hr> <p> </p> </td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0" height="40" vspace="0" hspace="0" align="center" bordercolor="0"> <tr bgcolor="#999999"> <td><img src="images/footer3.gif" width="600" height="40" align="right" vspace="0" hspace="0" usemap="#Map" border="0"> <map name="Map"> <area shape="rect" coords="491,4,593,38" href="index.html"><area shape="rect" coords="47,1,114,55" href="#top" target="_self"> </map></td> </tr> </table> <map name="Map2"> <area shape="rect" coords="255,12,334,36" href="spacecraft.html" alt="to Chronology section home"> <area shape="rect" coords="419,13,493,36" href="spacecraft_planetary_venus.html"> </map></body> </html>