Lambda 4S

From Wikipedia, the free encyclopedia

**Lambda 4S**
Size
L-4S-5
Function	Experimental carrier rocket
Manufacturer	ISAS Nissan
Country of origin	Japan
Height	16.5 metres (54 ft)
Diameter	0.74 metres (2 ft 5 in)
Mass	9,400 kilograms (20,700 lb)
Stages	Four
Capacity
Payload to LEO	26 kilograms (57 lb)^{[citation needed]}
Associated rockets
Family	Lambda
Derivatives	Lambda 4SC
Launch history
Status	Retired
Launch sites	Kagoshima Pad L
Total launches	5
Successes	1
Failures	4
First flight	26 September 1966
Last flight	11 February 1970
Notable payloads	Ōsumi

The Lambda 4S or L-4S was an experimental Japanese expendable carrier rocket. It was produced by Nissan and the Institute of Space and Astronautical Science and launched five times between 1966 and 1970 with Ōsumi technology demonstration satellites. The first four launches failed, however the fifth, launched on 11 February 1970, successfully placed Ōsumi-5, the first Japanese satellite, into orbit.^[1]^[2]

The Lambda 4S consisted of four stages, with two booster rockets augmenting the first stage. SB-310 rockets were used as boosters, with an L753 first stage. The second stage was a reduced length derivative of the L753, whilst an L500 was used as the third stage. The fourth stage was an L480S. All of the stages burned solid fuel.^[2]

The Lambda 4S could place 26 kilograms (57 lb) of payload into low Earth orbit. It was launched from the Kagoshima Space Centre. Following its retirement in 1970, a sounding rocket derived from it, the Lambda 4SC, flew three times. The Mu replaced Lambda for orbital launches.

References

↑ McDowell, Jonathan. "Lambda". Orbital and Suborbital Launch Database. Jonathan's Space Page. Retrieved 2009-05-08.
↑ 2.0 2.1 Wade, Mark. "Lambda". Encyclopedia Astronautica. Retrieved 2009-05-08.

External links

Japanese orbital launch systems

JAXA

Active	Epsilon H-IIA H-IIB

Planned	H-III

ISAS

Retired	Lambda (4S) Mu (4S 3C 3H 3S 3SII V)

NASDA

Retired	N-I‡ N-II‡ H-I‡ H-II

Other

Cancelled	GX‡

Retired	J-I

‡ Based around licence-produced US rockets

v t e Orbital launch systems

Current	Antares Ariane 5 Atlas V Delta II IV Dnepr-1 Epsilon Falcon 9 v1.1 GSLV H-IIA H-IIB Kuaizhou Long March 2C 2D 2F 3A 3B 3C 4B 4C Minotaur I IV V Pegasus Proton-M PSLV Rokot Safir Shavit Strela Soyuz U FG 2 2-1v Taurus Unha Vega VLS-1 Zenit 2M 3SL 3SLB 3F

Planned	Angara Ariane 6 Athena Ic IIc III Ausroc IV Falcon 9-R Falcon Heavy GSLV Mk III Haas Long March 5 6 7 9 11 LauncherOne Naro-2 RPS (420, 550) Simorgh SLS Southern Cross SPARK Tsyklon-4 VLM VLS-Alfa VLS-Beta

Retired	Ariane 1 2 3 4 ASLV Athena I II Atlas B D E/F G H I II III LV-3B SLV-3 Able Agena Centaur Black Arrow Conestoga Delta A B C D E G J L M N 0100 1000 2000 3000 4000 5000 III Diamant Energia Europa Falcon 1 Falcon 9 v1.0 Feng Bao 1 H-I H-II Juno I Juno II Kaituozhe-1 Kosmos 1 2I 3 3M Lambda 4S Long March 1 2A 2E 3 4A Mu 4S 3C 3H 3S 3SII V N1 N-I N-II Naro-1 Paektusan Pilot Proton UR-500 K R-7 Luna Molniya M L Polyot Soyuz L M U2 Soyuz/Vostok Sputnik Voskhod Vostok L K 2 2M Saturn I IB V INT-21 Scout Shtil' SLV Space Shuttle Sparta Start-1 Thor Able Ablestar Agena Burner Delta DSV-2U Thorad-Agena Titan II GLV IIIA IIIB IIIC IIID IIIE 34D 23G CT-3 IV Tsyklon 2 3 Vanguard Volna Zenit-2

This article is issued from Wikipedia. The text is available under the Creative Commons Attribution/Share Alike; additional terms may apply for the media files.

Lambda 4S

See also

References

External links