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2. Space One KAIROS - Wikipedia

   en.wikipedia.org/wiki/Space_One_KAIROS

   The KAIROS rocket (カイロスロケット), or Kii-based Advanced & Instant Rocket System, [1] is a Japanese solid-fuel rocket designed to launch small satellites of mass up to 250 kg to low Earth orbit and up to 150 kg to sun-synchronous orbit by the private spaceflight company Space One. [2]

3. Aerojet Rocketdyne AR1 - Wikipedia

   en.wikipedia.org/wiki/Aerojet_Rocketdyne_AR1

   The Aerojet Rocketdyne AR1 is a 2,200-kilonewton-class (500,000 lbf) thrust RP-1/LOX oxidizer-rich staged combustion cycle rocket engine project. [1]The engine was conceived in 2014, and received US government funding to build a prototype engine in 2016. [2]

4. 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.

5. RL10 - Wikipedia

   en.wikipedia.org/wiki/RL10

   The RL10 is a liquid-fuel cryogenic rocket engine built in the United States by Aerojet Rocketdyne that burns cryogenic liquid hydrogen and liquid oxygen propellants. Modern versions produce up to 110 kN (24,729 lb f) of thrust per engine in vacuum. RL10 versions were produced for the Centaur upper stage of the Atlas V and the DCSS of the Delta IV

6. AOL.com - News, Sports, Weather, Entertainment, Local & Lifestyle

   www.aol.com

   AOL latest headlines, entertainment, sports, articles for business, health and world news.

7. Astrobee - Wikipedia

   en.wikipedia.org/wiki/Astrobee

   The three-stage Astrobee 1500 (first stage: Recruit, second stage: Aero jet, third stage: Alcor) has a ceiling of 1000 km, a takeoff thrust of 566 kN, a takeoff weight of 5200 kg, a diameter of 0.79 m and a length of 10.40 m. [4]