Míša

Míša is a popular Czech brand of frozen confection. Míšas have been made continuously since 1961, and sell over 12 million ice pops per year, making it the most successful ice cream brand in the Czech Republic. It has survived events such as the Velvet Revolution and is fondly remembered as an integral part of Czech childhood.

They are made with frozen cream cheese, rather than ice cream or yogurt.

The logo features a grinning green bear, holding its arms above the word "Míša."

See also

References

Mia

Mia, MIA, or M.I.A. may refer to:

Airports

Government and politics

Mía (Armando Manzanero song)

"Mía" ("Mine") is a song by Mexican songwriter Armando Manzanero included in the album A Mi Amor Con Mi Amor (1967). It was first released as a double-side single along with the track "Felicidad" in 1969.

On March 20, 2001 a new version of the song was recorded as a duet with Spanish singer Miguel Bosé and was included on Manzanero's album Duetos. In 2006, Bosé also included this track on his album Papito. Popular Mexican singers like José José and Luis Miguel have performed "Mía" live on several occasions.

Mia was also performed by Los Trios Los Panchos in LP called "El Trio Los Panchos y Armando Manzanero". It included 11 songs composed by Armando Manzanero. "Contigo Aprendi, Perdoname, Cuando Estoy Contigo, Llevatela, Quiero Para Ti, Esta Tarde Vi Llover, No, Adoro, Mia, La Casa and Voy A Pagar La Luz."

References

DM

DM, Dm, dm, or D.M. may stand for:

Academic titles

Business and products

S1.5400

The S1.5400 (GRAU Index 11D33) was a Soviet single nozzle liquid propellant rocket engine burning liquid oxygen and kerosene in an oxidizer rich staged combustion cycle. It was the first rocket engine to use this cycle in the world, and it was designed by V. M. Melnikov, an alumnus of Isaev, within Korolev's Bureau, for the Molniya fourth stage, the Block-L. It was also the first Soviet engine designed for start and restart in vacuum, and had the highest isp at the time of its deployment.

Its development took from 1958 to 1960. The first production run was started on May 1960, and it passed all the firing tests. Its first flight failed before the Block-L was activated and it was in a Venera flight during 1961 that it had its first success. Between 1961 and 1964 it went through an improvement program that ended up in the S1.5400A1 version (GRAU Index 11D33M). It improved thrust from 63.74 kilonewtons (14,330 lbf) to 66.69 kilonewtons (14,990 lbf) and isp from 338.5s to 340s, while keeping weight the same.

RD-253

The RD-253 (Russian: Раке́тный дви́гатель 253, Rocket Engine 253) and its later variants, the RD-275 and RD-275M, are liquid-propellant rocket engines developed in the Soviet Union by Energomash. The engines are used on the first stage of the Proton launch vehicle and use an oxidizer-rich staged combustion cycle to power the turbopumps. The engine burns UDMH/N₂O₄, which are highly toxic but hypergolic and storable at room temperature, simplifying the design.

History

Development of RD-253 started in 1961. Preliminary investigations and development of the engine as well as its further production was performed under the guidance of Valentin Glushko and finished in 1963. The RD-253 uses a staged combustion cycle for oxidizer-rich generator gas. It was used for the first time in July 1965 year when six engines powered the first stage of the rocket. Development and production of RD-253 was a qualitative leap forward for rocketry of that time by achieving high levels of thrust, specific impulse and pressure in the combustion chamber. This engine is one of the most reliable engines in the USSR and modern Russia.