From sparkling skin to a better functioning brain, water fixes just about everything. Having your own water cooler means you’ll never struggle to stay hydrated.

With the Purity Series you will enjoy the improved taste of water for drinking, coffee, juice and ice cubes and any other drinking water use. RO water also enhances the flavour of food when cooking. Enjoy healthier water for your whole family.

Country: Russia. Launch Vehicles: R-1. Propellants: Lox/Alcohol. Stages: R-1 stage. Agency: Glushko bureau. Bibliography: 225, 287, 317, 321, 323, 342, 394. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use

We’ve got dozens of coolers looking for a family like yours and a place to call home. Let us match you with the perfect cooler.

Purity Reverse Osmosis systems are among the best appliances you can find on the market to improve water taste and quality. With the water quality of our environment worsening, we have been prompted to design and manufacture this compact, domestic RO purifier to meet these challenges with the highest quality solutions.

Around 1 million single-use plastic bottles are bought around the world every MINUTE. Do your bit in reducing plastic waste while hydrating your family with a water cooler that just tastes better.

Date: 1946-50. Number: 184 . Thrust: 304.00 kN (68,341 lbf). Unfuelled mass: 885 kg (1,951 lb). Specific impulse: 237 s. Specific impulse sea level: 203 s. Burn time: 65 s. Height: 3.70 m (12.10 ft). Diameter: 1.65 m (5.41 ft). German salaries and conditions were good - the chief of the German team receiving the second highest salary after the Soviet designer-in-chief. The RD-100 was built in 1946 at a former Ilyushin aviation plant that had been moved to Tashkent in World War 2 (now the Energomash factory). There was no equipment so everything had to be started from scratch. By mid-1947 the first RD-100 was ready. In May 1948 the first RD-100 test took place at Khimki itself, with the spectators watching from 1 km away. There are still tests at the same location but thrust levels are now 800 metric tons force. The R-1 rocket with the RD-100 engine entered service in 1950. Thrust (sl): 267.000 kN (60,023 lbf). Thrust (sl): 27,227 kgf. Engine: 885 kg (1,951 lb). Chamber Pressure: 15.90 bar. Propellant Formulation: Lox/Alcohol-75%. Thrust to Weight Ratio: 35.3672316384181. Oxidizer to Fuel Ratio: 1.28. Country: Russia. Launch Vehicles: R-1. Propellants: Lox/Alcohol. Stages: R-1 stage. Agency: Glushko bureau. Bibliography: 225, 287, 317, 321, 323, 342, 394. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use

Thrust (sl): 267.000 kN (60,023 lbf). Thrust (sl): 27,227 kgf. Engine: 885 kg (1,951 lb). Chamber Pressure: 15.90 bar. Propellant Formulation: Lox/Alcohol-75%. Thrust to Weight Ratio: 35.3672316384181. Oxidizer to Fuel Ratio: 1.28. Country: Russia. Launch Vehicles: R-1. Propellants: Lox/Alcohol. Stages: R-1 stage. Agency: Glushko bureau. Bibliography: 225, 287, 317, 321, 323, 342, 394. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use

German salaries and conditions were good - the chief of the German team receiving the second highest salary after the Soviet designer-in-chief. The RD-100 was built in 1946 at a former Ilyushin aviation plant that had been moved to Tashkent in World War 2 (now the Energomash factory). There was no equipment so everything had to be started from scratch. By mid-1947 the first RD-100 was ready. In May 1948 the first RD-100 test took place at Khimki itself, with the spectators watching from 1 km away. There are still tests at the same location but thrust levels are now 800 metric tons force. The R-1 rocket with the RD-100 engine entered service in 1950. Thrust (sl): 267.000 kN (60,023 lbf). Thrust (sl): 27,227 kgf. Engine: 885 kg (1,951 lb). Chamber Pressure: 15.90 bar. Propellant Formulation: Lox/Alcohol-75%. Thrust to Weight Ratio: 35.3672316384181. Oxidizer to Fuel Ratio: 1.28. Country: Russia. Launch Vehicles: R-1. Propellants: Lox/Alcohol. Stages: R-1 stage. Agency: Glushko bureau. Bibliography: 225, 287, 317, 321, 323, 342, 394. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use

Country: Russia. Launch Vehicles: R-1. Propellants: Lox/Alcohol. Stages: R-1 stage. Agency: Glushko bureau. Bibliography: 225, 287, 317, 321, 323, 342, 394. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use

Thrust (sl): 267.000 kN (60,023 lbf). Thrust (sl): 27,227 kgf. Engine: 885 kg (1,951 lb). Chamber Pressure: 15.90 bar. Propellant Formulation: Lox/Alcohol-75%. Thrust to Weight Ratio: 35.3672316384181. Oxidizer to Fuel Ratio: 1.28. Country: Russia. Launch Vehicles: R-1. Propellants: Lox/Alcohol. Stages: R-1 stage. Agency: Glushko bureau. Bibliography: 225, 287, 317, 321, 323, 342, 394. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use