|
gptkbp:instance_of
|
gptkb:shotgun
gptkb:satellite
|
|
gptkbp:action
|
semi-automatic
|
|
gptkbp:analysis
|
post-mission analysis
|
|
gptkbp:barrel_length
|
18.5 in
|
|
gptkbp:barrel_type
|
smoothbore
|
|
gptkbp:caliber
|
12 gauge
|
|
gptkbp:collaboration
|
gptkb:NASA_and_ESA
|
|
gptkbp:collaborations
|
international research institutions
|
|
gptkbp:collection
|
various scientific data
|
|
gptkbp:communication_system
|
S-band
|
|
gptkbp:control_system
|
autonomous
|
|
gptkbp:controls
|
reaction wheels
|
|
gptkbp:cooling_system
|
passive and active systems
|
|
gptkbp:country_of_origin
|
gptkb:Italy
|
|
gptkbp:crew
|
STS-7 crew
|
|
gptkbp:data_transmission
|
downlink to ground stations
|
|
gptkbp:design
|
1 year
|
|
gptkbp:design_date
|
gptkb:1978
|
|
gptkbp:design_features
|
pistol grip
folding stock
integrated rail system
|
|
gptkbp:disbandment_date
|
1984-04-24
|
|
gptkbp:feed_system
|
gptkb:magazine
|
|
gptkbp:first_flight
|
gptkb:1983
|
|
gptkbp:historical_significance
|
used in various conflicts
popular in the 1980s and 1990s
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SPAS-1
|
|
gptkbp:impact
|
contributed to microgravity research
|
|
gptkbp:launch_date
|
1983-04-18
|
|
gptkbp:launch_mass
|
2,500 kg
|
|
gptkbp:launch_price
|
estimated $100 million
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Space_Shuttle_Challenger
|
|
gptkbp:launch_window
|
April 1983
|
|
gptkbp:legacy
|
paved the way for future SPAS missions
|
|
gptkbp:length
|
1,020 mm
|
|
gptkbp:magazine_capacity
|
8 rounds
|
|
gptkbp:manufacturer
|
gptkb:Mc_Donnell_Douglas
Franchi
|
|
gptkbp:material
|
collapsible stock
|
|
gptkbp:mission
|
gptkb:Johnson_Space_Center
successful
data for future missions
|
|
gptkbp:mission_duration
|
7 days
|
|
gptkbp:mission_type
|
gptkb:scientific_research
|
|
gptkbp:muzzle_velocity
|
400 m/s
|
|
gptkbp:notable_users
|
gptkb:Italian_Army
gptkb:French_Gendarmerie
gptkb:U._S._military
various police forces
|
|
gptkbp:objective
|
microgravity research
technology demonstration
|
|
gptkbp:operational_period
|
1983-1984
|
|
gptkbp:operational_status
|
decommissioned
|
|
gptkbp:operations
|
gas-operated
|
|
gptkbp:orbit_type
|
gptkb:112
low Earth orbit
|
|
gptkbp:orbital_inclination
|
28.5 degrees
|
|
gptkbp:orbital_period
|
90 minutes
eventual reentry
|
|
gptkbp:payload_capacity
|
gptkb:scientific_instruments
1,000 kg
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:range
|
50 m
|
|
gptkbp:rate_of_fire
|
6 rounds per minute
|
|
gptkbp:recoil
|
low recoil
|
|
gptkbp:recovery_method
|
splashdown
|
|
gptkbp:related_model
|
gptkb:Benelli_M4
gptkb:Franchi_SPAS-12
gptkb:Franchi_SPAS-15
gptkb:Mossberg_500
|
|
gptkbp:safety
|
manual safety
|
|
gptkbp:scientific_goals
|
study effects of microgravity
|
|
gptkbp:scientific_instruments
|
various experiments
|
|
gptkbp:sights
|
iron sights
|
|
gptkbp:speed
|
1984-04-24
controlled descent
|
|
gptkbp:successor
|
gptkb:SPAS-2
gptkb:SPAS-12
|
|
gptkbp:trigger_type
|
single-action
|
|
gptkbp:type
|
combat shotgun
|
|
gptkbp:used_by
|
gptkb:law_enforcement
gptkb:military
|
|
gptkbp:variant
|
SPAS-1, SPAS-12
|
|
gptkbp:weight
|
3.5 kg
|
|
gptkbp:year_established
|
gptkb:1979
|
|
gptkbp:bfsParent
|
gptkb:STS-51-D
gptkb:STS-24
gptkb:STS-16
gptkb:STS-11
gptkb:STS-41_B
|
|
gptkbp:bfsLayer
|
5
|