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  2. Comparison of orbital launcher families - Wikipedia

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

    Manufac.: Main manufacturer; Payload: Maximum mass of payload, for 3 altitudes LEO, low Earth orbit; GTO, geostationary transfer orbit; TLI, trans-Lunar injection; Cost: Price for a launch at this time, in millions of US$ Launches reaching... Total: Flights which lift-off, or where the vehicle is destroyed during the terminal count

  3. Comparison of orbital launch systems - Wikipedia

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

    Vehicle Origin Manufacturer Height Maximum payload mass (kg) Reusable / Expendable Orbital launches including failures [a] Launch site(s) Dates of flight LEO GTO Other First Latest Angara A5 / Briz-M Russia: Khrunichev: 48.7 m 24,500 [1] 5,200 [1] 2,800 to GEO [1] Expendable: 2 [1] Plesetsk, Vostochny: 2014 2020 Angara-1.2 Russia: Khrunichev ...

  4. Comparison of orbital rocket engines - Wikipedia

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

    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 AJ-10-190 USA: Aerojet: Space Shuttle, Orion, Apollo CSM: Active Upper N 2 O 4 /MMH: Pressure-fed: 316 [1] 26,689 [1] 8.62 [1] 118 [1] 23.08: Archimedes New Zealand USA: Rocket Lab ...

  5. List of spacecraft manufacturers - Wikipedia

    en.wikipedia.org/wiki/List_of_spacecraft...

    manufacturer of Antares, Minotaur and Pegasus: PLD Space: Spain manufacturer of Miura 1 and Miura 5 Rocket Lab: New Zealand/United States 46/50: manufacturer of Electron launch vehicle Space One: Japan manufacturer of the KAIROS launch vehicle SpaceX: United States 426/434: Falcon 1, Falcon 9, Falcon Heavy and Starship: Sea Launch: United ...

  6. Comparison of solid-fuelled orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_solid...

    Vehicle Main stages Origin Manufacturer Height (meter) Diameter (meter) Weight (ton) Mass to... (kg) Maiden flight Retired Record Status Solid Liquid LEO Other orbit Ares I: 1 1 United States: Alliant Techsystems / Boeing: 94 5.5 25000 (2015) 0/0 Cancelled Athena I: 2 1 United States: Lockheed Martin: 1995 2001 3/4 Retired Athena Ic: 2 1 United ...

  7. Comparison of crewed space vehicles - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_crewed_space...

    Manufacturer Altitude Launch system Crew size Length (m) Diameter (m) Launch mass (kg) Power system Generated power (W) Recovery method First spaceflight § Last spaceflight Flights § SpaceShipOne USA: Scaled Composites: 112 km X Prize: White Knight Hybrid Motor: 1: 8.53 8.05 3,600 Batteries Runway landing 2004: 2004: 3 [note 22] X-15 USA ...

  8. List of orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/List_of_orbital_launch_systems

    ISRO's launch vehicles. Left to right: SLV, ASLV, PSLV, GSLV, LVM3 RLV Human Rated Launch Vehicle (HRLV) Vikram series, the under development orbital class launch family of Skyroot Aerospace in comparison with already flown Vikram S, the sounding rocket ISRO/DoS systems. SLV-3 – Retired; Augmented Satellite Launch Vehicle (ASLV) – Retired

  9. Comparison of retired orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_retired...

    Vehicle Origin Manufacturer Height Mass to ... (kg) Reuse Launches (+ suborbital) Launch Sites Date of flight LEO GTO Other First Last Antares 110–130 United States: Orbital: 40.5-41.9 m 5,100 [1] 1,500 to SSO No 5 [1] MARS: 2013 2014 Antares 230 / 230+ United States: Northrop Grumman: 42.5 m 8,200 [1] 3,000 to SSO [a] No 13 MARS: 2016 2023 ...