Compartment. 2MV-1: Venera 2MV-1 No.1 (Sputnik 19), Venera 2MV-1 No.2 (Sputnik 20) 2MV-2: Venera 2MV-2 No.1 (Sputnik 21) 2MV-4: Mars 2MV-4 No.1 (Sputnik...

Mars 2MV-4 No.1 also known as Sputnik 22 in the West, was a Soviet spacecraft, which was launched in 1962 as part of the Mars programme, and was intended...

Venera 2MV-1 No.1 Sputnik 20 – Venera 2MV-1 No.2 Sputnik 21 – Venera 2MV-2 No.1 Sputnik 22 – Mars 2MV-4 No.1 Sputnik 23 – Mars 1 Sputnik 24 – Mars 2MV-3 No...

Mars 2MV-3 No.1 also known as Sputnik 24 in the West, was a Soviet spacecraft, which was launched in 1962 as part of the Mars program, and was intended...

Venera 2MV-1 No.2, also known as Sputnik 20 in the Western world, was a Soviet spacecraft, which was launched in 1962 as part of the Venera programme...

Venera 2MV-1 No.1, also known as Sputnik 19 in the West, was a Soviet spacecraft, which was launched in 1962 as part of the Venera programme. Due to a...

Mars. Two other Soviet launches at around the same time, Mars 2MV-4 No.1 and Mars 2MV-3 No.1 were 900-kilogram (2,000 lb) spacecraft, however both failed...

Mars 2MV-4 can refer to two Soviet spacecraft: Mars 2MV-4 No.1 Mars 1 Mars 2M (disambiguation) This disambiguation page lists articles associated with...

Venera 2MV-2 No.1, also known as Sputnik 21 in the West, was a Soviet spacecraft, which was launched in 1962 as part of the Venera programme, and was...

{\displaystyle I(U,s)={\frac {3A{\sqrt {2mV_{a}}}}{2s}}({\frac {e}{h}})^{2}U\exp(-{\frac {4{\pi }s}{h}}{\sqrt {2mV_{a}}})} where V a {\displaystyle V_{a}}...

Mars 1, also known as 1962 Beta Nu 1, Mars 2MV-4 and Sputnik 23, was an automatic interplanetary station launched in the direction of Mars on November...

| p 2 − p 1 | = 2 m v {\displaystyle |\mathbf {p} _{2}-\mathbf {p} _{1}|=2mv} . The magnitude of the change of momentum of all molecules that bounce off...

Baikonur LC-1/5 Venera (2a) (2MV-1 #1, Sputnik 19) Partial failure 01.09.1962 Molniya T103-13 Baikonur LC-1/5 Venera (2b) (2MV-1 #2, Sputnik 20) Partial...

(650 ft/min) Armament Rockets: 8 x RS-82 rockets. (UT-2MV) Bombs: 2-4 x 50 kg (110 lb) bombs (UT-2MV) Aircraft of comparable role, configuration, and era...

unmanned probes to Mars and Venus. It was an incremental improvement of earlier 2MV probes and was used for Zond 1, Zond 2 and Zond 3 missions to Mars as well...

defined as follows: v 0 = 2 m V 0 a 2 ℏ 2 {\displaystyle v_{0}={\sqrt {\frac {2mV_{0}a^{2}}{\hbar ^{2}}}}} These definitions can be inserted in the expression...

case. Whereby l = k 2 + 2 m V 0 ℏ 2 {\displaystyle l={\sqrt {k^{2}+{\frac {2mV_{0}}{\hbar ^{2}}}}}} is the (increased) wave number of the plane wave inside...

— Venera 2MV-1 No.1 2MV-1 No.1 Atmospheric probe 25 August 1962 — — Escape stage failed; Re-entered three days later — Venera 2MV-1 No.2 2MV-1 No.2 Atmospheric...

improvements based on experience with earlier missions. It was superseded by the 2MV family. Mars 1M: Mars probe 1M No.1 (failure), Mars probe 1M No.2 (failure)...

ka=n\pi -\sin ^{-1}\left({\frac {k\hbar }{\sqrt {2mV_{1}}}}\right)-\sin ^{-1}\left({\frac {k\hbar }{\sqrt {2mV_{2}}}}\right)} where n = 1 , 2 , 3 , … {\displaystyle...

Inclination 0.58° Period 311 days Flyby of Venus Closest approach 19 May 1961 Distance 100,000 km (62,000 mi) Venera ← Tyazhely Sputnik Venera 2MV-1 No.1 →...

latter, capable of two firings, was a lighter version of that used on the 2MV model with higher specific impulse and longer burn time. During this mission...

Failed launches Mars 1M No.1 1M No.2 2MV-4 No.1 2MV-3 No.1 Mariner 3 Mars 2M No.521 2M No.522 Mariner 8 Mars 3MS No.170 Mars 96 Fobos-Grunt / Yinghuo-1...

temperature readings. The silicon diodes have temperature dependency of -2mV per degree Celsius. Thus the junction temperature can be determined by passing...

beginning with MMV All pages with titles containing MMV M2V, see M V star 2MV MVV (disambiguation) MV (disambiguation) MMU (disambiguation) This disambiguation...

deflection angle:: 111  Δ P = 2 m v ⋅ sin ⁡ θ 2 . {\displaystyle \Delta P=2mv\cdot \sin {\frac {\theta }{2}}.} A second formula for Δ P {\displaystyle...

Linear particle accelerators. Linear Particle Accelerator (LINAC) Animation by Ionactive 2MV Tandetron linear particle accelerator in Ljubljana, Slovenia...

the tail of the aircraft. Pe-2M Variant of Pe-2I with heavier armament. Pe-2MV This version was armed with 20 mm ShVAK cannons and two 12.7 mm (0.5 in)...

Earth; destroyed by range safety following guidance failure Atlas-LV3 Agena-B 2MV-1 No.1 25 August 1962 OKB-1  Soviet Union Lander Launch failure Premature...

Landing site Region Status Country MOLA Entry velocity References 1. Mars 2MV-3 No.1 04 Nov 1962 25 Nov 1962 890 - - Failure  Soviet Union - - 2. Mars...