Atlas D

In-active Atlas

Convair ()

April 14, 1959

Description

The SM-65D Atlas, or Atlas D, was the first operational version of the U.S. Atlas missile. Atlas D was first used as an intercontinental ballistic missile (ICBM) to deliver a nuclear weapon payload on a suborbital trajectory. It was later developed as a launch vehicle to carry a payload to low Earth orbit on its own, and later to geosynchronous orbit, to the Moon, Venus, or Mars with the Agena or Centaur upper stage.

Specifications
  • Stages
    1
  • Length
    25.15 m
  • Diameter
    3.0 m
  • Fairing Diameter
    3.0 m
  • Launch Mass
    119 T
  • Thrust
    1880 kN
Family
  • Name
    Atlas D
  • Family
    Atlas
  • Variant
    D
  • Alias
  • Full Name
    SM-65D Atlas
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
    1400 kg
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity

Convair

Commercial
None
1943

Convair, previously Consolidated Vultee, was an American aircraft manufacturing company that later expanded into rockets and spacecraft. The company was formed in 1943 by the merger of Consolidated Aircraft and Vultee Aircraft. In 1953 it was purchased by General Dynamics, and operated as their Convair Division for most of its corporate history.

Atlas D | OV1-11,12,86

Convair | USA
Vandenberg SFB, CA, USA
July 27, 1967, 7 p.m.
Status: Launch Failure
Mission:

The OV1 (Orbiting Vehicle 1) were small research satellite to be launched piggy back on Atlas ICBM test flights. They consisted in general of the OV1 satellite and the OV1-PM propulsion module (or upper stage) to reach orbit.

Low Earth Orbit
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Atlas D | OV1-9 & 10

Convair | USA
Vandenberg SFB, CA, USA
Dec. 11, 1966, 9:09 p.m.
Status: Launch Successful
Mission:

The OV1 (Orbiting Vehicle 1) were small research satellite to be launched piggy back on Atlas ICBM test flights. They consisted in general of the OV1 satellite and the OV1-PM propulsion module (or upper stage) to reach orbit.

Low Earth Orbit
Explore Share

Atlas D | OV1-7

Convair | USA
Vandenberg SFB, CA, USA
July 14, 1966, 2:10 a.m.
Status: Launch Successful
Mission:

The OV1 (Orbiting Vehicle 1) were small research satellite to be launched piggy back on Atlas ICBM test flights. They consisted in general of the OV1 satellite and the OV1-PM propulsion module (or upper stage) to reach orbit.

Low Earth Orbit
Explore Share

Atlas D | OV1-4 & 5

Convair | USA
Vandenberg SFB, CA, USA
March 30, 1966, 9:20 a.m.
Status: Launch Successful
Mission:

The OV1 (Orbiting Vehicle 1) were small research satellite to be launched piggy back on Atlas ICBM test flights. They consisted in general of the OV1 satellite and the OV1-PM propulsion module (or upper stage) to reach orbit.

Low Earth Orbit
Explore Share

Atlas D | OV1-2

Convair | USA
Vandenberg SFB, CA, USA
Oct. 5, 1965, 9:07 a.m.
Status: Launch Successful
Mission:

The OV1 (Orbiting Vehicle 1) were small research satellite to be launched piggy back on Atlas ICBM test flights. They consisted in general of the OV1 satellite and the OV1-PM propulsion module (or upper stage) to reach orbit.

Low Earth Orbit
Explore Share

Atlas D | OV1-3

Convair | USA
Vandenberg SFB, CA, USA
May 28, 1965, 2:54 a.m.
Status: Launch Failure
Mission:

The OV1 (Orbiting Vehicle 1) were small research satellite to be launched piggy back on Atlas ICBM test flights. They consisted in general of the OV1 satellite and the OV1-PM propulsion module (or upper stage) to reach orbit.

Low Earth Orbit
Explore Share

Atlas D | FIRE 2

Convair | USA
Cape Canaveral, FL, USA
May 22, 1965, 9:55 p.m.
Status: Launch Successful
Mission:

FIRE (Flight Investigation of Re-Entry) was a high-speed reentry heat research program to obtain data on materials, heating rates, and radio signal attenuation on spacecraft reentering the atmosphere at speeds of about 24,500 miles per hour.

Suborbital
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Atlas D | OV1-1

Convair | USA
Vandenberg SFB, CA, USA
Jan. 21, 1965, 9:34 p.m.
Status: Launch Failure
Mission:

The OV1 (Orbiting Vehicle 1) were small research satellite to be launched piggy back on Atlas ICBM test flights. They consisted in general of the OV1 satellite and the OV1-PM propulsion module (or upper stage) to reach orbit.

Low Earth Orbit
Explore Share

Atlas D | FIRE 1

Convair | USA
Cape Canaveral, FL, USA
April 14, 1964, 9:42 p.m.
Status: Launch Successful
Mission:

FIRE (Flight Investigation of Re-Entry) was a high-speed reentry heat research program to obtain data on materials, heating rates, and radio signal attenuation on spacecraft reentering the atmosphere at speeds of about 24,500 miles per hour.

Suborbital
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Falcon 9
Success
3 days, 3 hours ago
Starlink Group 6-54
Space Launch Complex 40 - Cape Canaveral, FL, USA

A batch of 23 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.


Falcon 9
Success
4 days, 1 hour ago
Galileo L12 (FOC FM25 & FM27)
Launch Complex 39A - Kennedy Space Center, FL, USA

Two satellites for Europe's Galileo navigation system. Originally planned for launch on Soyuz-ST and then Ariane 6 but both were unavailable. Gali…


Long March 2
Success
6 days, 13 hours ago
Shenzhou 18
Launch Area 4 (SLS-1 / 921) - Jiuquan Satellite Launch Center, People's Republic of China

Seventh crewed flight to the Chinese space station.


Electron
Success
1 week, 1 day ago
Beginning Of The Swarm (ACS3 & NeonSat-1)
Rocket Lab Launch Complex 1B - Onenui Station, Mahia Peninsula, New Zealand

NASA's Advanced Composite Solar Sail System (ACS3) is a technology demonstration mission tasked with deploying a composite boom solar sail. NeonSa…


Falcon 9
Success
1 week, 1 day ago
Starlink Group 6-53
Space Launch Complex 40 - Cape Canaveral, FL, USA

A batch of 23 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.