President Dwight D. Eisenhower approved the recommendations of his Advisory Committee on Government Organization that the "leadership of the civil space effort be lodged in a strengthened and redesignated National Advisory Committee for Aeronautics," and that legislation be enacted to "give NACA the authority and flexibility" to carry out its expanded responsibilities.

The Office of the Secretary of Defense, in the first significant forward step to accelerate development of a space capability, reiterated the space role of the Air Force. In addition to its missile programs the Air Force was responsible for the 117L system and "... has a recognized long term development responsibility for manned space flight capability with the primary objective of accomplishing satellite flight as soon as technology permits." Furthermore, the Air Force was told it was to carry forward and accelerate the Atlas 117L project "under the highest national priority in order to attain an initial operational capability in the earliest possible date," But the proposed interim system using a Thor booster combined with a second stage and recoverable capsule "should not be pursued. " The Department of Defense did agree that a Thor booster with a suitable second stage "may be the most promptly and readily available device for experimental flights with laboratory animals" and development of such hardware including a system for recovery of animals was authorized. (Msg 03-014, Cmdr ARDC, to Cmdr AFBMD, 5 Mar 58.)

Due to technical problems and the launch failure of a Zenit spy satellite, the launch of the dual Vostoks is pushed back to April. Therefore a trip to New York by the cosmonauts in March will not be possible. In any case the Presidium has decided against allowing them to address the United Nations.

NASA announced an American agreement with Australia, signed on February 26, that permitted the space agency to build and operate several new tracking stations "down under." A key link in the Jet Propulsion Laboratory's network of Deep Space Instrumentation Facilities would be constructed in Tidbinbilla Valley, 18 kilometers (11 miles) southwest of Canberra. Equipment at this site included a 26-meter (85-foot) parabolic dish antenna and electronic equipment for transmitting, receiving, and processing radio signals from spacecraft. Tracking stations would be built also at Carnarvon and Darwin.

Before GLV and spacecraft were electrically mated, the launch vehicle's status was reverified with a Combined Systems Test (CST) performed on March 10. A special series of Electronic-Electrical Interference (EEI) Tests began March 12 and ended March 25. Evaluation of test results confirmed that the intent of EEI testing had been accomplished, despite some persistent anomalies. A successful post-EEI systems reverification CST was performed March 27.

Only on this day does Kamanin receive a copy of Korolev's "Preliminary Plan for Voskhod spacecraft (3KV and 3KD) series in 1965", issued in February. His plan is:

• 3KV Number 5 - to be completed in June, launched by August, an unmanned biological flight with life forms, to be kept in orbit for 15-30 days, with experimental equipment in the cabin to monitor the organisms and a self-destruct system
• 3KV Number 6 - to be completed in August, and flown by October on a 15-day mission with a two-man crew: a flight commander and scientist
• 3KV number 7 - to be completed in December, and flown by April 1966 on a 15-20 day mission with a pilot and physician aboard. The spacecraft would also conduct artificial gravity experiments for 3-4 days of the flight
• 3KD numbers 8 and 9 - a prime spacecraft and a backup, fitted with the airlock system. A spacecraft commander and pilot would make a flight or flights of 3 to 5 days. 2 or 3 spacewalks would be conducted on each flight, with the EVA cosmonaut using a manoeuvring apparatus to back away as far as 50 to 100 m from the spacecraft. Manually controlled landing of the capsule would also be demonstrated

Kamanin is preparing the final press packet, with the cosmonaut biographies, which will be delivered to TASS but only released by them after confirmation that the spacecraft is in orbit. Later Kamanin and forty other guests, including hero-cosmonauts and future hero-cosmonauts, throw a party for Tereshkova's 28th birthday. There is tension in the room as the cosmonauts eye each other as competitors for the flights after Voskhod-2. Volynov is the leading candidate to command the next flight, and has already been a back-up four times, but Marshal Rudenko keeps blocking his selection for flight (Volynov is a Jew). Rudenko is pushing Beregovoi for the next flight, and everyone in the room knows it...

The Institute of Medical-Biological Problems (IMBP) and the Zvezda design bureau (designer of the ejection seat, space suits, and environmental control system for the Vostok spacecraft) became partners with OKB-1 in developing the SOZh closed-loop environemental control system. An earth-based simulator - the Earth Experimental Complex (NEK) was built. V Ulibishev, G Manovtsev, and A Bozhko spent an entire year in this closed-environment test unit beginning on 5 March 1967. An analogous US experiment was conducted for only 90 days in July-September 1970.

The second SV-5D Precision Recovery Including Maneuvering Reentry (PRIME) lifting body was successfully launched from Vandenberg by an Atlas booster. Although the SV-5D was not recovered, its on-board sensors provided excellent data on the effects of reentry. This was also the first spacecraft to perform cross-range maneuvers during reentry. The X-23A SV-5D lifting body vehicle demonstrated a 1055 km cross-range manoeuvre, but again air snatch failed.

The L1 reaches its apogee. The time comes to attempt the third midcourse manoeuvre. There are three attempts to orient the spacecraft. The first was at the minimum sensitivity setting for the star tracker, the second at the maximum setting, and the third using a high-density filter. Sirius is finally acquired the third time. The spacecraft is oriented and makes a 15 second burn with a 9.129 m/s delta-V (versus 9.202 m/s planned). This is good enough to assure the spacecraft will hit the re-entry corridor without a further correction.

Kamanin is still fighting the issue of mission length - he doesn't want to risk lives. Soyuz 9 landed virtually in the laps of the doctors, but what if they had made an emergency landing in the ocean, or taiga? They were in no condition to save themselves before assistance arrived. Every day over 20-22 days is a risk to the life of the crew, in Kamanin's view. Smirnov, Serbin, Mishin - they don't care about this.

Meanwhile the doctor's verdict is in on Shonin. He is to be sent to a sanatorium for rehabilitation.

AMSAT-OSCAR 8 was launched piggyback with LandSat 3 (ERTS 3) and PIX. The third phase 2 satellite (Phase II-D). Weight 27.2 kg. Box shaped, 33 cm high, 38 x 38 cm. Circularly polarized VHF canted turnstile, UHF quarter wave monopole, and HF half-wave dipole antenna system. Another cooperative international effort (United States, Canada, Germany and Japan). AO-8 had a similar store-and-forward service as AO-7 and carried Mode A (145.850-900 MHz uplink and 29.400-500 MHz downlink) and Mode J (145.900-146.000 MHz uplink and 435.100 MHz downlink (inverted)) linear transponders and telemetry beacons on 435.095 MHz and 29.402 MHz. AO-8's primary mission was for educational applications and amateur communications. It was in operation for six years until the battery failed on June 24, 1983.

Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Launch vehicle put payload into geosynchronous transfer orbit Positioned in geosynchronous orbit at 32 deg E in 1982; 63 deg E in 1982; 27 deg W in 1983-1985; 34 deg W in 1985-1992; 40 deg W in 1992; 31 deg W in 1993-1995; 29 deg W in 1995 As of 1 September 2001 located at 4.64 deg W drifting at 3.747 deg W per day. As of 2007 Mar 7 located at 4.34W drifting at 3.748W degrees per day.

X-38 atmospheric test vehicle V-132 was dropped from carrier plane NB-52 # 8 at 16:17 GMT. The V-132 subscale version of the X-38 successfully deployed its parafoil and glided to a landing on the lakebed after a 9 minute flight. V-132 tested the rudders and flaps; the simpler V-131, which made two drop tests earlier, tested the parafoil control system.

NASA's long-delayed WIRE (Wide Field Infrared Explorer) astronomy satellite was the fifth Small Explorer (SMEX) mission managed by NASA-Goddard. The L-1011 Stargazer launch aircraft took off from Vandenberg's runway 30/12 at 01:55 GMT on March 2 for the first launch attempt. The planned 02:56 GMT launch was cancelled at T-46 seconds due to a problem with the tail fin release mechanism of the Pegasus XL launch vehicle. The second attempt was successful, with the Pegaus XL being dropped at 36 degrees N x 123 degrees W over the Pacific Ocean at 02:56 GMT. However the WIRE ran into serious trouble shortly after orbit injection. The cover of the solid hydrogen telescope ejected prematurely, and the cryogenic coolant evaporated and vented, spinning the satellite out of control. WIRE was going to make an infrared photometry survey, generating a large catalog of galaxies and quasars. Air dropped in Point Arguello WADZ.

Expedition 8 Commander Michael Foale today reestablished a vacuum between the Destiny Laboratory's science window's two panes of optical-quality glass. The window work was associated with continuing repairs following a small pressure leak detected on the International Space Station in January. Additional Details: here....

In the COL (Columbus Orbital Laboratory), FE-2 Leo Eyharts had an hour allotted to perform troubleshooting on a structural element which earlier (2/17) had prevented installation of a K-BAR (Knee-Brace Assembly Replacement) capture mechanism on the overhead F2 rack, as required for relocating of the MSG (Microgravity Science Glovebox) and EXPRESS Rack 3 (ER3). Additional Details: here....

Second unmanned Orbital Test Vehicle X-37B reusable spaceplane. Possibly placed in a 400 x 420 km x 40 deg orbit like that used by OTV-1; mission expected to last 9 months with automatic landing at Vandenberg Air Force Base. The Centaur AV-026 upper stage was deorbited over the Indian Ocean on the first orbit.