Apollo–Soyuz Docking Module

E238196

The Apollo–Soyuz Docking Module was a specially designed adapter spacecraft that enabled the American Apollo and Soviet Soyuz vehicles to physically connect and support joint operations during the first international crewed space mission.

All labels observed (2)

Label Occurrences
ASTP Docking Module 1
Apollo–Soyuz Docking Module canonical 1

How this entity was disambiguated

Statements (49)

Predicate Object
instanceOf docking module ⓘ
spacecraft ⓘ
spacecraft adapter ⓘ
agreementContext developed under 1972 US–USSR space cooperation agreement ⓘ
alsoKnownAs Apollo–Soyuz Docking Module ⓘ
surface form: ASTP Docking Module
atmosphereAdaptation adapted Apollo pure oxygen atmosphere to Soyuz nitrogen–oxygen atmosphere ⓘ
connectsWith Apollo spacecraft ⓘ
Soyuz spacecraft ⓘ
control primarily controlled from Apollo command module ⓘ
countryOfOrigin United States of America ⓘ
surface form: United States
crewAccess allowed transfer of astronauts and cosmonauts between spacecraft ⓘ
crewCapacity passage for up to three crew at a time ⓘ
developmentAgency Johnson Space Center ⓘ
surface form: NASA Manned Spacecraft Center
diameter approximately 1.4 meters ⓘ
displayStatus no complete flight article on public display ⓘ
dockingDate 1975-07-17 ⓘ
dockingSystemType androgynous docking system ⓘ
feature airlock between Apollo and Soyuz ⓘ
androgynous peripheral attach system docking mechanism ⓘ
environmental control system ⓘ
pressure equalization system ⓘ
translation and rotation control thrusters ⓘ
heritage influenced later international docking standards ⓘ
historicalSignificance enabled first international crewed space docking ⓘ
symbol of US–Soviet détente in space ⓘ
launchDate 1975-07-15 ⓘ
launchSite Kennedy Space Center Launch Complex 39B ⓘ
launchVehicle Saturn IB ⓘ
length approximately 3.15 meters ⓘ
manufacturer Rockwell International ⓘ
surface form: North American Rockwell

Rockwell International ⓘ
mass approximately 2,000 kilograms ⓘ
mission Apollo–Soyuz Test Project ⓘ
surface form: Apollo–Soyuz Test Project mission
missionDuration about 9 days ⓘ
operator NASA ⓘ
partOf Apollo–Soyuz Test Project ⓘ
powerSource electrical power from Apollo spacecraft ⓘ
precededBy Apollo docking systems used with lunar module ⓘ
program Apollo program ⓘ
Soviet space program ⓘ
surface form: Soviet crewed space program
purpose enable docking between Apollo and Soyuz spacecraft ⓘ
support joint US–Soviet crewed space operations ⓘ
reentryDate 1975-07-24 ⓘ
role provided structural interface between Apollo and Soyuz ⓘ
served as an airlock between different cabin atmospheres ⓘ
status mission completed ⓘ
successor APAS-89 docking system conceptually ⓘ
usedOnMission Apollo spacecraft CSM-111 ⓘ
Soyuz 19 ⓘ

How these facts were elicited

Referenced by (2)

Full triples — surface form annotated when it differs from this entity's canonical label.

Apollo–Soyuz Test Project → usedDockingModule → Apollo–Soyuz Docking Module ⓘ
Apollo–Soyuz Docking Module → alsoKnownAs → Apollo–Soyuz Docking Module ⓘ
this entity surface form: ASTP Docking Module