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2. Comparison of orbital rocket engines - Wikipedia

   en.wikipedia.org/wiki/Comparison_of_orbital...

   Engine Origin Designer Vehicle Status Use Propellant Power cycle Specific impulse (s) [a] Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [b] Oxidiser: fuel ratio

3. Rocketdyne - Wikipedia

   en.wikipedia.org/wiki/Rocketdyne

   Rocketdyne's Solid Propulsion Operations business unit was engaged in the development, testing and production of solid rocket engines at McGregor, Texas for nearly twenty years. The Rocket Fuels Division of Phillips Petroleum Company began using the former Bluebonnet Ordnance Plant in 1952. In 1958, Phillips and Rocketdyne entered a partnership ...

4. Super heavy-lift launch vehicle - Wikipedia

   en.wikipedia.org/wiki/Super_heavy-lift_launch...

   A super heavy-lift launch vehicle is a rocket that can lift to low Earth orbit a "super heavy payload", which is defined as more than 50 metric tons (110,000 lb) [1] [2] by the United States and as more than 100 metric tons (220,000 lb) by Russia. [3]

5. Blackburn Shark - Wikipedia

   en.wikipedia.org/wiki/Blackburn_Shark

   The Blackburn T.9 Shark has its origins within the early 1930s as a private venture by the company. [2] Originally known as the Blackburn T.S.R., standing for torpedo-spotter-reconnaissance, it was designed in conformance with Air Ministry Specification S.15/33, which sought a combined torpedo-(naval artillery) spotter-reconnaissance aircraft for the Fleet Air Arm (FAA).

6. Vikas (rocket engine) - Wikipedia

   en.wikipedia.org/wiki/Vikas_(rocket_engine)

   The Vikas (a portmanteau from initials of VIKram Ambalal Sarabhai [5] [6]) is a family of hypergolic liquid fuelled rocket engines conceptualized and designed by the Liquid Propulsion Systems Centre in the 1970s. [7] [8] The design was based on the licensed version of the Viking engine with the chemical pressurisation system. [9]

7. Comparison of orbital launch systems - Wikipedia

   en.wikipedia.org/wiki/Comparison_of_orbital...

   The following chart shows the number of launch systems developed in each country, and broken down by operational status. Rocket variants are not distinguished; i.e., the Atlas V series is only counted once for all its configurations 401–431, 501–551, 552, and N22.