This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com Luna 8K72

Luna LV
Luna LV -

Credit: © Mark Wade. 1,088 bytes. 70 x 246 pixels.



Family: R-7. Country: Russia. Status: Hardware. Other Designations: Luna. Library of Congress Designation: A-1. Department of Defence Designation: SL-3. Article Number: 8K72.

R-7 ICBM with single-engine upper stage used for early Soviet unmanned lunar shots.


Specifications

Launches: 9. Failures: 6. Success Rate: 33.33% pct. First Launch Date: 23 September 1958. Last Launch Date: 19 April 1960. Payload: 280 kg. to a: translunar trajectory. Liftoff Thrust: 403,477 kgf. Total Mass: 277,000 kg. Core Diameter: 2.6 m. Total Length: 30.8 m.


Luna 8K72 Chronology


1958 Mar 20 -
1958 Aug 18 - LV Configuration: Luna 8K72 B1-3. Launch Site: Baikonur .
1958 Sep 2 -
1958 Sep 23 - LV Configuration: Luna 8K72 s/n B1-3. Launch Site: Baikonur . Launch Complex: LC1. FAILURE: Launcher disintegrated 93 seconds after launch due to longitudinal resonance of strap-ons.
1958 Oct 11 - - 08:42 GMT. LV Configuration: Luna 8K72 s/n B1-4. Launch Site: Baikonur . Launch Complex: LC1. FAILURE: Launcher disintegrated 104 seconds after launch due to longitudinal resonance of strap-ons.
1958 Dec 4 - LV Configuration: Luna 8K72 s/n B1-5. Launch Site: Baikonur . Launch Complex: LC1. FAILURE: Core engines shut off at 245 seconds into the flight. Cause was a loss of lubrication to the hydrogen peroxide pump.
1959 Jan 2 - - 16:41 GMT. LV Configuration: Luna 8K72 s/n B1-6. Launch Site: Baikonur . Launch Complex: LC1.
1959 Jun 18 - LV Configuration: Luna 8K72 s/n I1-7. Launch Site: Baikonur . Launch Complex: LC1. FAILURE: Inertial system failed at 153 seconds after launch. Vehicle destroyed by range safety.
1959 Sep 12 - - 06:39 GMT. LV Configuration: Luna 8K72 s/n I1-7B. Launch Site: Baikonur . Launch Complex: LC1.
1959 Oct 4 - - 02:30 GMT. LV Configuration: Luna 8K72 s/n I1-8. Launch Site: Baikonur . Launch Complex: LC1.
1960 Apr 15 - LV Configuration: Luna 8K72 s/n L1-9. Launch Site: Baikonur . Launch Complex: LC1. FAILURE: The third stage RO-5 engine either did not reach full thrust or shut down early.
1960 Apr 19 - LV Configuration: Luna 8K72 s/n L1-9A. Launch Site: Baikonur . Launch Complex: LC1. FAILURE: Strap-on B reached only 75 percent of thrust at ignition. Four tenths of a second after liftoff it broke away from the core and the rocket exploded.

Bibliography:



Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .