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        <li>Thursday, 23 May 2013</li>
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<div id="contentwrapper"><div id="rightcontent"><div id="headimage"><img height="100" width="530" alt="National Space Science Data Center Header" src="/logo/nssdc_header.jpg"/></div><h1>Sputnik  7</h1><p><strong>NSSDC/COSPAR ID:</strong> 1961-002A</p><div class="twocol"><div class="urone"><h2>Description</h2><p>
          This was the first Soviet attempt at a Venus probe. The probe was successfully launched into Earth orbit with a SL-6/A-2-e (Molniya 8K78) launcher. The launch payload consisted of an Earth orbiting launch platform (Tyazheliy Sputnik 4) and the Venera probe. The fourth stage (a Blok L Zond rocket) was supposed to launch the Venera probe towards a landing on Venus after one Earth orbit but ignition failed, probably due to a fault in the power supply to the guidance system, the PT-200 DC transformer had not been designed to work in a vacuum. The spacecraft and launch platform remained attached in a 212 x 318 km, 64.95 degree inclination, 89.8 minute Earth orbit. Because of its large size (6483 kg), the mission was originally thought by non-Soviet observers to be a failed manned mission, and later was described as a test of an Earth orbiting platform from which an interplanetary probe could be launched. This was the first attempt to launch a spacecraft from a preliminary Earth orbit. The orbit decayed and the spacecraft reentered the Earth's atmosphere on 26 February after 22 days.
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The Venera probe had a mass of about 645 kg and was based on the M1 (Mars) spacecraft design. It was designed as a Venus atmospheric probe. It carried a 3-axis magnetometer, a variometer (vertical speed indicator), and charged particle monitors. It also carried a small globe which held medallions and other commemorations of the mission. The spacecraft communications were at 66 and 66.2 MHz.
          </p></div><div class="urtwo"><h2>Alternate Names</h2><ul><li>Tyazheliy Sputnik 4</li><li>00071</li></ul><h2>Facts in Brief</h2><p><strong>Launch Date:</strong> 1961-02-04<br/><strong>Launch Vehicle:</strong> Modified SS-6 (Sapwood) with 2nd Generation Upper Stage + Escape Stage<br/><strong>Launch Site:</strong> Tyuratam (Baikonur Cosmodrome), U.S.S.R<br/><strong>Mass:</strong> 6843.0 kg<br/></p><h2>Funding Agency</h2><ul><li>Unknown (U.S.S.R)</li></ul><h2>Disciplines</h2><ul><li>Engineering</li><li>Planetary Science</li></ul><h2>Additional Information</h2><ul><li><a href="spacecraftOrbit.do?id=1961-002A">Launch/Orbital information for Sputnik  7</a></li><li><a href="spacecraftPdmp.do?id=1961-002A">PDMP information for Sputnik  7</a></li><li><a href="spacecraftTelemetry.do?id=1961-002A">Telecommunications information for Sputnik  7</a></li></ul><ul><li><a href="experimentSearch.do?spacecraft=Sputnik  7">Experiments on Sputnik  7</a></li><li><a href="datasetSearch.do?spacecraft=Sputnik  7">Data collections from Sputnik  7</a></li></ul><h2/><p>
          Questions or comments about this spacecraft can be directed to:
          <a href="mailto:David.R.Williams@nasa.gov?Subject=NMC Comment/Question: Sputnik  7 (1961-002A)">Dr. David R. Williams</a>.
          </p></div></div><div class="clear"> </div><h2>Selected References</h2><p>Shelton, W.,
      Soviet space exploration - the first decade,
      Arthur Barker Ltd., Unnumbered, London, England, 1969.
      </p><p>Harvey, B.,
      The new Russian space programme from competition to collaboration,
      John Wiley &#x26; Sons, Chichester, England, 1996.
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        <li>NASA Official: <a href="mailto:Edwin.J.Grayzeck@nasa.gov">Dr. Ed Grayzeck</a></li>
        <li>Curator: <a href="mailto:Ed.Bell@nasa.gov">E. Bell, II</a></li>
        <li>Version 4.0.22, 21 May 2013</li>
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