Jump to content

KSR-2 (sounding rocket)

From Wikipedia, the free encyclopedia

(Redirected from KARI KSR-2)

KSR-II at a launchpad

KSR-2 (Korean Sounding Rocket-2) is a South Korean sounding rocket designed by KARI.

Spec

Payload: 150 kg
Apogee: 160 km
Thrust: 86 kN
Weight: 2000 kg
Diameter: 0.42 m
Length: 11.04 m
Launch: July 9, 1997 (1st)/June 11, 1998 (2nd)^[1]

See also

General references

KSR-II on Encyclopedia Astronautica

References

^ "Scientific Rocket". kari.re.kr.

South Korean space program

Organizations

Korea AeroSpace Administration (KASA)
Korea Aerospace Research Institute (KARI)
Korea Astronomy and Space Science Institute (KASI)

Launch sites

Sounding rockets

KARI	KSR-I KSR-II KSR-III Nuri TLV
ADD	Solid-Fuel Space Launch Vehicle TLV[1]

Launch vehicles

KARI	Naro-1 (KSLV-I) Nuri (KSLV-II) KSLV-III (In development)
ADD	Solid-Fuel Space Launch Vehicle[2]

Kitsat
- 1
- 2
- 3
KOMPSAT
- 1
- 2
- 3
- 3A
- 5
- 6
- 7
- 7A
STSat
- 1
- 2A
- 2B
- 2C
- 3
KOREASAT
- 1
- 2
- 3
- 5
- 5A
- 6
- 7
CAS500
- 1
- 2
GEO-KOMPSAT
- 1
- 2A
- 2B
- 3

Korea Pathfinder Lunar Orbiter

Contractors

Astronauts

Related institutions

Agency for Defense Development (ADD)
KAIST Satellite Technology Research Center (SaTReC)
National Space Committee
ROKAF space operations center

This Korea-related article is a stub. You can help Wikipedia by expanding it.

This rocketry article is a stub. You can help Wikipedia by expanding it.

Retrieved from "https://en.wikipedia.org/w/index.php?title=KSR-2_(sounding_rocket)&oldid=1252679897"

Hidden category:

All stub articles

pFad - Phonifier reborn

Pfad - The Proxy pFad of © 2024 Garber Painting. All rights reserved.

Note: This service is not intended for secure transactions such as banking, social media, email, or purchasing. Use at your own risk. We assume no liability whatsoever for broken pages.

Alternative Proxies:

Alternative Proxy