H-II A Mitsubishi
by Motormike
uploaded 2018-04-03
24 downloads /
1
points
VAB
mod ship

Details

  • Type: VAB
  • Class: ship
  • Part Count: 15
  • Mods: 2

Mods

  • CONTARES
  • TweakScale - Rescale Everything!

Description

¨H-IIA¨H IIA No. F23 with GPM on its way to the launchpad.jpg¨H-IIA No. F23 rolls out to the launch pad in February 2014¨Function Medium-lift launch vehicle¨Manufacturer ¨Mitsubishi Heavy Industries (prime)¨ATK (sub)¨Country of origin Japan¨Cost per launch US$90 million[1]¨Size¨Height 53 m (174 ft)¨Diameter 4 m (13 ft)¨Mass 285,000–445,000 kg (628,000–981,000 lb)¨Stages 2¨Capacity¨Payload to LEO 10,000–15,000 kg (22,000–33,000 lb)¨Payload to GTO 4,100–6,000 kg (9,000–13,200 lb)¨Associated rockets¨Family H-II¨Derivatives H-IIB¨Launch history¨Status Active¨Launch sites Tanegashima LA-Y¨Total launches ¨38 202: 24 204: 4 2022: 3 2024: 7¨Successes ¨37 202: 24 204: 4 2022: 3 2024: 6¨Failures 1 (2024)¨First flight ¨202: 29 August 2001¨204: 18 December 2006¨2022: 26 February 2005¨2024: 4 February 2002¨Last flight ¨202: 27 February 2018¨204: 19 August 2017¨2022: 14 September 2007¨2024: 23 February 2008¨Notable payloads ¨SELENE Ibuki Akatsuki¨Boosters (All variants) – SRB-A¨No. boosters 2–4¨Thrust 2,260 kN (510,000 lbf)¨Total thrust 4,520–9,040 kN (1,020,000–2,030,000 lbf)¨Specific impulse 280 seconds (2.7 km/s)¨Burn time 120 seconds¨Fuel HTPB¨Boosters (2022 / 2024) – Castor 4AXL¨No. boosters 2–4¨Thrust 745 kN (167,000 lbf)¨Total thrust 1,490–2,980 kN (330,000–670,000 lbf)¨Specific impulse 280 seconds (2.7 km/s)¨Burn time 60 seconds¨Fuel Solid¨First stage¨Engines 1 LE-7A¨Thrust 1,098 kN (247,000 lbf)¨Specific impulse 440 seconds (4.3 km/s)¨Burn time 390 seconds¨Fuel LOX / LH2¨Second stage¨Engines 1 LE-5B¨Thrust 137 kN (31,000 lbf)¨Specific impulse 447 seconds (4.38 km/s)¨Burn time 534 seconds¨Fuel LOX / LH2¨¨Liftoff of H-IIA Flight 19¨¨H-IIA rocket lineup¨¨H-IIA¨H-IIA (H2A) is an active expendable launch system operated by Mitsubishi Heavy Industries (MHI) for the Japan Aerospace Exploration Agency. The liquid-fueled H-IIA rockets have been used to launch satellites into geostationary orbit, to launch a lunar orbiting spacecraft, and to launch Akatsuki, which studied the planet Venus. Launches occur at the Tanegashima Space Center. The H-IIA first flew in 2001. As of December 2017, H-IIA rockets were launched 37 times, including 31 consecutive missions without a failure, dating back to November 29, 2003.

A mod rocket called H-II A Mitsubishi. Built with 15 of the finest parts, its root part is RK.SAS.1500.

Built in the VAB in KSP version 1.4.2.

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