LK-700

{{Short description|Soviet moon lander program}}{{Infobox spacecraft class

| image =

| name = LK-700

| manufacturer = OKB-52

| country = Soviet Union

| applications = Land cosmonauts on the Moon and bring them back to Earth

| operator = Soviet space program

| lifetime =

| derivedfrom = LK-1

| derivatives = TKS spacecraft

| status = Canceled

| built =

| launched =

| retired =

}}

LK-700 was a Soviet direct ascent lunar lander program proposed in 1964.{{cite web|url=http://www.astronautix.com/craft/lk700.htm|title=LK-700|work=astronautix.com|accessdate=5 July 2015|url-status=dead|archiveurl=https://web.archive.org/web/20131121214206/http://www.astronautix.com/craft/lk700.htm|archivedate=21 November 2013}} It was developed by Vladimir Chelomey as an alternative to the N1-L3 program. It was also a further development of the LK-1 lunar flyby spacecraft.

It would have been launched using the proposed UR-700{{Cite web|url=https://www.russianspaceweb.com/ur700.html|title = UR-700 launch vehicle}} rocket (related to the Proton rocket) with a crew of three cosmonauts on a direct flight to the lunar surface and back.

The direct landing approach would allow the Soviets to land anywhere on the moon's nearside.{{cite web|url=http://news.discovery.com/space/history-of-space/what-would-a-soviet-moon-landing-have-looked-like-130722.htm|title=What Would a Soviet Moon Landing Have Looked Like?|work=DNews|accessdate=5 July 2015|archive-date=3 May 2016|archive-url=https://web.archive.org/web/20160503002347/http://news.discovery.com/space/history-of-space/what-would-a-soviet-moon-landing-have-looked-like-130722.htm|url-status=dead}} The program was canceled in 1974.

Mission profile

Uncrewed flights would be followed by crewed flights. The proposed schedule was:

  • May 1972: First UR-700/LK-700 uncrewed launch. Subsequent launches in November 1972 and April 1973.
  • April 1973: First crewed UR-700/LK-700 launch. Subsequent flights in August and October 1973.

Following initial LK-700 landings, the more ambitious Lunar Expeditionary Complex (LKE) would be delivered to the surface in three UR-700 launches:

  • Launch 1: lunar station to enable a six-month stay
  • Launch 2: LK-700 with crew
  • Launch 3: large rover

Characteristics

  • Crew size: 3
  • Orbital storage: 45 days
  • Spacecraft delta v: 9,061 m/s
  • Gross mass: 154,000 kg
  • Height: 21.20 m
  • Span: 2.70 m
  • Thrust: 131.40 kN
  • Specific impulse: 326 s

References