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STKR-46
|
RPOD operations shall be monitorable from the customer ground station
|
|
16/Mar/26 3:01 PM
|
16/Mar/26 3:01 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-45
|
The IOR System shall comply with applicable planetary protection and contamination control guidelines for missions operating beyond Earth orbit.
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|
16/Mar/26 2:53 PM
|
16/Mar/26 2:53 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-44
|
The IOR System and associated missions shall comply with national licensing and regulatory authorization requirements for launch, on-orbit operations, and space servicing activities.
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|
16/Mar/26 2:53 PM
|
16/Mar/26 2:53 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-43
|
The IOR propellant delivery system shall be capable of refueling IOR depots as well as other depots implementing compatible standardized refueling interfaces.
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|
16/Mar/26 2:40 PM
|
16/Mar/26 2:40 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-42
|
An IOR propellant depot shall be capable of being refuelled by any compatible standardized propellant delivery system.
|
|
16/Mar/26 2:39 PM
|
16/Mar/26 2:39 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-41
|
The IOR architecture shall support multiple propellant depots deployed across different orbital regimes (e.g., LEO, GEO, Earth-Moon L1/L2, and Lunar Orbit).
|
|
16/Mar/26 2:39 PM
|
16/Mar/26 2:39 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-40
|
The IOR system shall support autonomous Rendezvous, Proximity Operations and Docking (RPOD) and propellant transfer operations.
|
|
16/Mar/26 2:38 PM
|
16/Mar/26 2:38 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-39
|
The IOR system shall be capable of servicing IOR-Cooperative spacecraft, utilizing cooperative RPOD sequences coordinated between the servicing system and the client spacecraft.
|
|
16/Mar/26 2:37 PM
|
16/Mar/26 2:37 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-38
|
The IOR system shall be capable of servicing IOR-Aware spacecraft, utilizing closed-loop operational feedback provided by the client spacecraft to enhance RPOD and refuelling operations.
|
|
16/Mar/26 2:36 PM
|
16/Mar/26 2:36 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-37
|
The IOR system shall support servicing of the three spacecraft categories defined in the Mission Objectives: Interface-Enabled, IOR-Aware, and IOR-Cooperative spacecraft.
|
|
16/Mar/26 2:35 PM
|
16/Mar/26 2:35 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-36
|
RPOD operations shall be monitorable and controllable from the owner ground station.
|
|
14/Mar/26 1:43 PM
|
14/Mar/26 1:43 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-35
|
RPOD operations including propellant transfer, detachment, and departure shall be executable through autonomous and/or ground-controlled methods.
|
|
14/Mar/26 1:42 PM
|
14/Mar/26 1:42 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-34
|
The IOR system shall support servicing of passive third-party spacecraft fitted with an approved fuel interface.
|
|
14/Mar/26 1:41 PM
|
14/Mar/26 1:41 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-33
|
The SV shall perform active RPOD functions to cooperative, passive client spacecraft equipped with an approved fuel interface.
|
|
14/Mar/26 1:40 PM
|
14/Mar/26 1:40 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-32
|
The SV shall have the capability to perform Rendezvous, Proximity Operations, and Docking (RPOD).
|
|
14/Mar/26 1:28 PM
|
14/Mar/26 1:28 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-31
|
The IOR System shall ensure compliance with Orbital Debris Mitigation Standard Practices (ODMSP) as applicable
|
|
14/Mar/26 1:00 PM
|
14/Mar/26 1:00 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-30
|
The solution shall comply with CNSSP No. 12 as applicable.
|
|
14/Mar/26 1:00 PM
|
14/Mar/26 1:00 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-29
|
The SV shall be manufactured and qualified in accordance with applicable National Security Space Launch Port Launch Users Guide requirements.
|
|
14/Mar/26 12:59 PM
|
14/Mar/26 12:59 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-28
|
The SV shall adhere to recognized industry standards and best practices for on-orbit servicing.
|
|
14/Mar/26 12:58 PM
|
14/Mar/26 12:58 PM
|
Unassigned
|
Salman Javed
|
To Do
|
|
STKR-27
|
The Customer requires the IOR system to achieve a propellant transfer rate of not less than X kg per minute.
|
|
14/Mar/26 12:53 PM
|
16/Mar/26 3:41 PM
|
Unassigned
|
Salman Javed
|
To Do
|
