{| border="2" cellpadding="4" cellspacing="0" align="right" style="margin: 0 0 1em 1em; background: #f9f9f9; border: 1px #aaa solid; border-collapse: collapse; font-size: 95%;" |+S-IVB |- |colspan="2" align="center"|
S-IVB-206 which was used for the Skylab 2 flight |- !colspan="2" cellspacing="0" cellpadding="2" bgcolor="#FFDEAD"|Fact sheet |- |Height||17.8 m (58.4 ft) |- |Diameter||6.6 m (21.7 ft) |- |Mass||119,900 kg
(253,000 lb) |- |Engines||1 J-2 (rocket engine) engines |- |Thrust||1,001 kN
(225,000 lbf) |- |Fuel||liquid hydrogen and LOX |} The S-IVB (sometimes S4b) was built by the Douglas Aircraft Company and served as the third stage on the Saturn V and second stage on the Saturn IB. It had one J-2 engine. For lunar mission it was used twice: first for the orbit insertion after second stage cutoff, and then for the trans lunar injection (TLI) when the timing was right. ==History== The S-IVB evolved from the upper stage of the Saturn I rocket, the S-IV, and was the first stage of the Saturn V to be designed. The S-IV used a cluster of six engines but used the same fuels as the S-IVB - LH2 and LOX. It was also orginally meant to be the fourth stage of a planned rocket called the C-4, hence the name S-IV. Eleven companies submitted proposals for being the lead contractor on the stage by the deadline of 29 February, 1960. NASA administrator T. Keith Glennan decided on 19 April that Douglas Aircraft Company would be awarded the contract. Convair had come a close second but Glennan did not want to monopolise the liquid hydrogen fuelled rocket market as Convair was already building the Centaur rocket stage In the end the Marshall Space Flight Center decided to use the C-5 rocket (later called the Saturn V), which had three stages and would be topped with an uprated S-IV called the S-IVB which instead of using a cluster of engines would have a single J-2 engine. Douglas was awarded the contract for the S-IVB basically because of the similarities between it and the S-IV. At the same time it was decided to create the C-IB rocket (Saturn IB) that would also use the S-IVB as its second stage and could be used for testing the Apollo spacecraft in Earth orbit. Douglas built two distinct versions of the S-IVB, the 200 series and the 500 series. The 200 series was used by the Saturn IB and differed from the 500 in the fact that it did not have a flared interstage and had less helium pressurisation onboard as it would not be restarted. The S-IVB carried 72,700 liters (20,000 U.S. gallons) of LOX and 229,000 liters (63,000 U.S. gallons) of LH2. An un-used S-IVB provided the hull for Skylab, the United States first space station. During Apollo 13, Apollo 14, Apollo 15, Apollo 16 and Apollo 17, the S-IVB was crashed into the Moon in order to perform seismic measurement used for characterizing the lunar core.
''Three versions of the SIV/SIVB''
See other meanings of words starting from letter:
Words begining with S-IVB:
S-IVB
S-IVB_(rocket_stage)
S-IVB
{| border="2" cellpadding="4" cellspacing="0" align="right" style="margin: 0 0 1em 1em; background: #f9f9f9; border: 1px #aaa solid; border-collapse: collapse; font-size: 95%;" |+S-IVB |- |colspan="2" align="center"|
S-IVB-206 which was used for the Skylab 2 flight |- !colspan="2" cellspacing="0" cellpadding="2" bgcolor="#FFDEAD"|Fact sheet |- |Height||17.8 m (58.4 ft) |- |Diameter||6.6 m (21.7 ft) |- |Mass||119,900 kg
(253,000 lb) |- |Engines||1 J-2 (rocket engine) engines |- |Thrust||1,001 kN
(225,000 lbf) |- |Fuel||liquid hydrogen and LOX |} The S-IVB (sometimes S4b) was built by the Douglas Aircraft Company and served as the third stage on the Saturn V and second stage on the Saturn IB. It had one J-2 engine. For lunar mission it was used twice: first for the orbit insertion after second stage cutoff, and then for the trans lunar injection (TLI) when the timing was right. ==History== The S-IVB evolved from the upper stage of the Saturn I rocket, the S-IV, and was the first stage of the Saturn V to be designed. The S-IV used a cluster of six engines but used the same fuels as the S-IVB - LH2 and LOX. It was also orginally meant to be the fourth stage of a planned rocket called the C-4, hence the name S-IV. Eleven companies submitted proposals for being the lead contractor on the stage by the deadline of 29 February, 1960. NASA administrator T. Keith Glennan decided on 19 April that Douglas Aircraft Company would be awarded the contract. Convair had come a close second but Glennan did not want to monopolise the liquid hydrogen fuelled rocket market as Convair was already building the Centaur rocket stage In the end the Marshall Space Flight Center decided to use the C-5 rocket (later called the Saturn V), which had three stages and would be topped with an uprated S-IV called the S-IVB which instead of using a cluster of engines would have a single J-2 engine. Douglas was awarded the contract for the S-IVB basically because of the similarities between it and the S-IV. At the same time it was decided to create the C-IB rocket (Saturn IB) that would also use the S-IVB as its second stage and could be used for testing the Apollo spacecraft in Earth orbit. Douglas built two distinct versions of the S-IVB, the 200 series and the 500 series. The 200 series was used by the Saturn IB and differed from the 500 in the fact that it did not have a flared interstage and had less helium pressurisation onboard as it would not be restarted. The S-IVB carried 72,700 liters (20,000 U.S. gallons) of LOX and 229,000 liters (63,000 U.S. gallons) of LH2. An un-used S-IVB provided the hull for Skylab, the United States first space station. During Apollo 13, Apollo 14, Apollo 15, Apollo 16 and Apollo 17, the S-IVB was crashed into the Moon in order to perform seismic measurement used for characterizing the lunar core.
''Three versions of the SIV/SIVB''
See other meanings of words starting from letter:
S
SB | SC | SD | SE | SF | SG | SH | SI | SJ | SK | SL | SM | SN | SO | SP | SR | SS | ST | SU | SW | SX | SY | SZ |Words begining with S-IVB:
S-IVB
S-IVB_(rocket_stage)
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