Mission Type: Orbiter
Launch Vehicle: Modified SS-6 (Sapwood) with 2nd-generation upper stage + escape stage, 8K78M (no. Ya716-58)
Launch Site: Tyuratam (Baikonur Cosmodrome), USSR, NIIP-5 / launch site 1
Spacecraft Mass: About 1,600 kg
Spacecraft Instruments: Unknown
Deep Space Chronicle: A Chronology of Deep Space and Planetary Probes 1958-2000, Monographs in Aerospace History No. 24, by Asif A. Siddiqi
National Space Science Data Center, http://nssdc.gsfc.nasa.gov/
Solar System Log by Andrew Wilson, published 1987 by Jane's Publishing Co. Ltd.
Luna 14 successfully entered lunar orbit at 19:25 UT on 10 April 1968. Initial orbital parameters were 160 x 870 km at 42 degrees inclination.
The primary goal of the flight was to test communications systems in support of the N1-L3 piloted lunar landing project. Ground tracking of the spacecraft's orbit also allowed controllers to accurately map lunar gravitational anomalies in order to predict trajectories of future lunar missions such as those of the LOK and LK lunar-landing vehicles.
Luna 14 also carried scientific instruments to study cosmic rays and charged particles from the sun, although few details have been revealed.