儲存液態氫的鋼瓶. 液氢（LH 2 ），也称液态氢，是由氢气经由降温而得到的液体。 液态氢须要保存在非常低的温度下（大约在20.268开尔文，-252.8℃） [a] 。 它通常被作为火箭发射的燃料。. 液态氢可作为储存氢气的一种方式，因为液态氢比气态氢省空间。

Liquid hydrogen (H 2 (l)) is the liquid state of the element hydrogen.Hydrogen is found naturally in the molecular H 2 form. [4]To exist as a liquid, H 2 must be cooled below its critical point of 33 K.However, for it to be in a fully liquid state at atmospheric pressure, H 2 needs to be cooled to 20.28 K (−252.87 °C; −423.17 °F). [5] A common method of obtaining liquid hydrogen involves ...

• LO2/LH2 2. nd. and 3. rd. Stages • 850,000 Gallon LH2 Storage • 10,000 GPM max flowrate • 900,000 Gallon LO2 Storage • 10,000 GPM max flowrate • At the time, the largest Cryogenic Systems in the world. 5. Image Credit: NASA Image Gallery

Study of fuel systems for LH2-fueled subsonic transport aircraftVolume 2. Final report, September 1976--December 1977 Final report, September 1976--December 1977 Technical Report · Sat Jul 01 00:00:00 EDT 1978

The second stage held 260,000 US gallons (984 000 liters) of LH2; the third stage had 66,770 US gallons (252 750 liters) of LH2 onboard. The Space Shuttle stored its hydrogen in the enormous brownish-orange External Tank (ET) recognized by anyone who watched a launch live or on video. Loaded into the ET for every shuttle launch was 390,000 US ...

Deliverable 6.1 –Handbook of hydrogen safety: Chapter on LH2 safety. Pre-normative REsearch for Safe use of Liquid Hydrogen (PRESLHY). 2. J. E. Hall, P. Hooker, D. Willoughby. Int. J. Hydrogen Energy, 2014, 38: 20547-20553. European Hydrogen Train the Trainer Programme for Responders Liquefied hydrogen (LH 2)

A preliminary assessment of the facilities and equipment which will be required at a representative airport is provided so liquid hydrogen LH2 can be used as fuel in long range transport aircraft in 1995-2000. A complete facility was conceptually designed, sized to meet the projected air traffic requirement. The facility includes the liquefaction plant, LH2, storage capability, and LH2 fuel ...

Results are presented for an experimental investigation of self-pressurization and thermal stratification of a 4.89 cu m liquid hydrogen (LH2) storage tank subjected to low heat flux (0.35, 2.0, and 3.5 W/sq m) under normal gravity conditions. Tests were performed at fill levels of 83 to 84 percent (by volume). The LH2 tank was representative of …

LH2. Despite criticism and early technical failures, the taming of liquid hydrogen proved to be one of NASA’s most significant technical accomplishments. . . . Hydrogen — a light and extremely powerful rocket propellant — has the lowest molecular weight of any known substance and burns with extreme intensity (5,500°F). In combination ...

LH2 Boiloff Rate and Hold Time Subscale Dewar-Tank took 1,259 min (~21 hrs) to boiloff 7 liters Average boiloff rate ~ 0.33 L/ hr or ~6.3e-6 kg/s Average 2.8 W of heat load (92% from top plate) LH2 pressure Anticipate ~90 days for 19kg LH2 Dewar-Tank to boil dry Approximately 1% per day boiloff LH2 at tangent No LH2 Remaining Subscale Unit